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Aerodynamics, Transonic

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• Aerodynamics
• High-speed aeronautics
• Sound pressure

• Aerodynamics, Transonic -- Computer programs
• Aerothermodynamics
• Transonic planes
• Transonic wind tunnels

• Transonic aerodynamics
• Trans-sonic aerodynamics
• Transonic speeds
• Aerodynamics of transonic flight

• Transonic flow analysis for rotors. (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by I-Chung Chang and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Integration of aft-fuselage-mounted flow-through engine nacelles on an advanced transport configuration at Mach numbers from 0.6 to 1.0 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Bernard J. Blaha and Lewis Research Center (page images at HathiTrust)
• Computer program for calculating full potential transonic, quasi-three-dimensional flow through a rotating turbomachinery blade row / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Charles A. Farrell, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• CAS22 - FORTRAN program for fast design and analysis of sock-free airfoil cascades using fictitious-gas concept / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by George S. Dulikravich, Helmut Sobieczy, Universities Space Research Association, DFVLR--Institute fur̈ Theoretische Strom̈ungsmechanik, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
• Computation of the transonic perturbation flow fields around two- and three-dimensional oscillating wings / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by W. H. Weatherill, James D. Sebastian, F. Edward Ehlers, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Perturbation solutions for transonic flow on the blade-to-blade surface of compressor blade rows / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Stephen S. Stahara, John R. Spreiter, D. S. Chaussee, Inc Neilsen Engineering and Research, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Effects of afterbody boattail design and empennage arrangement on aeropropulsive characteristics of a twin-engine fighter model at transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service,), by Linda S. Bangert, David E. Reubush, Laurence D. Leavitt, and Langley Research Center (page images at HathiTrust)
• Qualitative evaluation of a flush air data system at transonic speeds and high angles of attack / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service,), by Terry J. Larson and Ames Research Center (page images at HathiTrust)
• Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by James T. Howlett, Samuel R. Bland, and Langley Research Center (page images at HathiTrust)
• Effect of empennage arrangement on single-engine nozzle/afterbody static pressures at transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by William P. Henderson, James R. Burley, and Langley Research Center (page images at HathiTrust)
• The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : design overview / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service,), by Charles D. Harris, Cuyler W. Brooks, William D. Harvey, and Langley Research Center (page images at HathiTrust)
• Integration effects of pylon geometry on a high-wing transport plane / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1989), by John R. Carlson, Milton Lamb, and United States. National Aeronautics and Space Administration. Office of Management (page images at HathiTrust)
• Wing analysis using a transonic potential flow computational method / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by P. A. Henne, R. M. Hicks, Ames Research Center, McDonnell Douglas Corporation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Experimental and analytical transonic flutter characteristics of a geared-elevator configuration / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Charles L. Ruhlin, Richard A. Gregory, Robert V. Doggett, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Transonic aerodynamic characteristics of a tailless fixed-wing supersonic transport model / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1966), by Edward J. Ray, Robert T. Taylor, and Langley Research Center (page images at HathiTrust)
• Flight Reynolds number effects on a contoured boattail nozzle at subsonic speeds / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Roger Chamberlin and Lewis Research Center (page images at HathiTrust)
• Measurements of fluctuating pressure in a rectangular cavity in transonic flow at high Reynolds numbers / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by M. B. Tracy, Julio Chu, Elizabeth B. Plentovich, and Langley Research Center (page images at HathiTrust)
• Use of CYBER 203 and CYBER 205 computers for three-dimensional transonic flow calculations / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by N. Duane Melson, James D. Keller, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Influence of orbital-maneuvering-system fairings and rudder flare on the transonic aerodynamic characteristics of a space shuttle orbiter / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by James C. Ellison and Langley Research Center (page images at HathiTrust)
• Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Michael J. Mann, Charles E. Mercer, and Langley Research Center (page images at HathiTrust)
• Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Jack Nugent, Odis C. Pendergraft, and Ames Research Center (page images at HathiTrust)
• Effects of reset stators and a rotating, grooved stator hub on performance of a 1.92-pressure-ratio compressor stage / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by George W. Lewis, Lonnie Reid, Donald C. Urasek, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of casing treatment on overall performance of axial-flow transonic fan stage with pressure ratio of 1.75 and tip solidity of 1.5 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Walter M. Osborn, Royce D. Moore, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A simple method for converting frequency-domain aerodynamics to the time domain / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1980), by E. H. Dowell and Langley Research Center (page images at HathiTrust)
• A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Richard W. Barnwell, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Effects of tip clearance on overall performance of transonic fan stage with and without casing treatment / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Royce D. Moore, Walter Martin Osborn, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Plenum response to simulated disturbances of the model and fan inlet guide vanes in a transonic tunne / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1980), by Blair B. Gloss and Langley Research Center (page images at HathiTrust)
• Static and dynamic pressure measurements on a NACA 0012 airfoil in the Ames High Reynolds Number Facility / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by John B. McDevitt, Arthur F. Okuno, and Ames Research Center (page images at HathiTrust)
• Transonic off-design drag and performance of an axisymmetric inlet with 40 percent internal contraction on design / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by Richard R. Woollett, David A. Choby, Edward T. Meleason, and Lewis Research Center (page images at HathiTrust)
• Calculation of unsteady transonic flows with mild separation by viscous-inviscid interaction / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by James T. Howlett and Langley Research Center (page images at HathiTrust)
• Design and performance of a high-pressure-ratio, highly loaded axial-flow transonic compressor space / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by George W. Lewis, Edward R. Tysl, Lonnie Reid, and Lewis Research Center (page images at HathiTrust)
• Flight Reynolds number effects on a fighter-type, circular-arc - 19 ̊conic boattail nozzle at subsonic speeds / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Roger Chamberlin and Lewis Research Center (page images at HathiTrust)
• Transonic off-design drag and performance of three mixed-compression axisymmetric inlets / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Richard R. Woollett, David A. Choby, Edward T. Meleason, and Lewis Research Center (page images at HathiTrust)
• Updated users' guide for TAWFIVE with multigrid / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by N. Duane Melson and Craig L. Streett (page images at HathiTrust)
• The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : evaluation of initial perforated configuration / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Charles D. Harris and Langley Research Center (page images at HathiTrust)
• Performance of inlet stage of transonic compressor / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1976), by Donald C. Urasek, George W. Lewis, Ronald J. Steinke, and Lewis Research Center (page images at HathiTrust)
• Numerical study of transonic flow over oscillating airfoils using the full potential equation / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Koji Isogai and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Two dimensional transonic testing with splitter plates / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Sanford Davis, Bodapati Satyanarayana, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Computation of transonic boattail flow with separation / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Richard G. Wilmoth and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Detailed transonic flow field measurements about a supercritical airfoil section / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Francis X. Hurley and Ames Research Center (page images at HathiTrust)
• Longitudinal aerodynamic characteristics of a generic fighter model with a wing designed for sustained transonic maneuver conditions / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by James C. Ferris and Langley Research Center (page images at HathiTrust)
• Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by William G. Johnson, Acquilla S. Hill, and Langley Research Center (page images at HathiTrust)
• Performance characteristics of an isolated coannular plug nozzle at transonic speeds / ([Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, VA : Available from the National Technical Information Service, [1985]), by Charles E. Mercer, James R. Burley, and Langley Research Center (page images at HathiTrust)
• Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by John T. Batina and Langley Research Center (page images at HathiTrust)
• Investigation of a supersonic cruise fighter model flow field / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by David E. Reubush, E. Ann Bare, and Langley Research Center (page images at HathiTrust)
• Subsonic and transonic unsteady- and steady-pressure measurements on a rectangular supercritical wing oscillated in pitch / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Rodney H. Ricketts and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Theoretical and experimental flow fields for a supersonic cruise fighter forebody / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by Steven F. Yaros and Langley Research Center (page images at HathiTrust)
• Supercritical maneuvering fighter configuration : wind-tunnel investigation at Mach numbers of 0.60 to 0.95 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Michael J. Mann, Richard L. Campbell, Charles E. Mercer, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• The design of supercritical wings by the use of three-dimensional transonic theory / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1979), by Michael J. Mann and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Experimental study of wing leading-edge devices for improved maneuver performance of a supercritical maneuvering fighter configuration / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Michael J. Mann and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Improved method for calculating transonic velocities on blade-to-blade stream surfaces of a turbomachine / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Jerry R. Wood, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
• A method for modifying two-dimensional adaptive wind-tunnel walls including analytical and experimental verification / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Joel L. Everhart and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Evaluation of structural design concepts for an arrow-wing supersonic cruise aircraft / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by I. F. Sakata, G. W. Davis, Lockheed-California Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : drag euqations / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by Cuyler W. Brooks, William D. Harvey, and Charles D. Harris (page images at HathiTrust)
• High-transonic-speed transport aircraft study : summary report / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Robert M. Kulfan, Ames Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• High angle canard missile test in the Ames 11-foot transonic wind tunnel / (Washington : National Aeronautics and Space Adiministration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Richard G. Schwind and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Operational manual for two-dimensional transonic code TSFOIL / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Stephen S. Stahara, Ames Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Nielsen Engineering & Research (page images at HathiTrust)
• Analysis of a theoretically optimized transonic airfoil / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by M. E. Lores, George D. Shrewsbury, Kenneth P. Burdges, Ames Research Center, and Lockheed-Georgia Company (page images at HathiTrust)
• The practical application of a finite difference method for analyzing transonic flow over oscillating airfoils and wings / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by F. Edward Ehlers, James D. Sebastian, Boeing Commercial Airplane Company, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Correlation of data related to shock-induced trailing-edge separation and extrapolation to flight Reynolds number / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1979), by J. F. Cahill, P. C. Connor, Ames Research Center, and Lockheed-Georgia Company (page images at HathiTrust)
• A linear aerodynamic analysis for unsteady transonic cascades / ([Washington, D.C.?] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service, 1984]), by Joseph M. Verdon, Joseph R. Caspar, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
• Variants and extensions of a fast direct numerical Cauchy-Riemann solver, with illustrative applications / (Washington : Natural Aeronautics and Space Administration : Springfield, Va. : For sale by the National Technical Information Service, 1977), by E. Dale Martin, Harvard Lomax, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Shadowgraph study of the upper stage flow fields of some Saturn V study configurations in the transonic Mach number range / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1965]), by C. Dale Andrews, David R. Carlson, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Experimental investigation of the influence of the turbulent boundary layer on the pressure distribution over a rigid two-dimensional wavy wall / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1971]), by Lado Muhlstein, Richard G. Beranek, George C. Marshall Space Flight Center, and Ames Research Center (page images at HathiTrust)
• FORTRAN program for quasi-three-dimensional calculation of surface velocities and choking flow for turbomachine blade rows / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, [1971]), by Theodore Katsanis (page images at HathiTrust)
• Experimental investigation of the transonic flutter of simple thin truncated-cone panels / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Jean Gilman and Langley Research Center (page images at HathiTrust)
• Static longitudinal aerodynamic characteristics at transonic speeds and angles of attack up to 99° of a reentry glider having folding wing-tip panels / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Walter B. Olstad and Langley Research Center (page images at HathiTrust)
• Transonic and supersonic flutter trend investigation of a variable-sweep wing / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by John C. Stonesifer, Robert C. Goetz, and Langley Research Center (page images at HathiTrust)
• Effects of vertical-tail size and a ventral fin on the static lateral and directional stability derivatives of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Walter B. Olstad and Langley Research Center (page images at HathiTrust)
• Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Earl R. Keener and Flight Research Center (U.S.) (page images at HathiTrust)
• Transonic pressure distributions over protuberances and adjacent areas in proximity to the nose of a launch vehicle / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1966), by James A. Blackwell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation at transonic speeds of loading over a 30 deg sweptback wing of aspect ratio 3, taper ratio 0.2, and NACA 65A004 airfoil section mounted on a body / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Donald D. Arabian and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transonic wind-tunnel investigation of the static aerodynamic characteristics of several configurations of the Blue Scout launch vehicle / (Washington, D.C. : National Aeronautics and Space Administration, [1963]), by Thomas C. Kelly, Robert J. Keynton, and Langley Research Center (page images at HathiTrust)
• Some effects of control profile and control trailing-edge angle on the oscillating hinge-moment and flutter characteristics of flap-type controls at transonic speeds / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by William C. Moseley, Thomas G. Gainer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance, stability, and control characteristics at transonic speeds of three V/STOL airplane configurations with wings of variable sweep / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Arvo A. Luoma, William J. Alford, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of some effects of flexibility on the lift and pitching-moment characteristics of a series of low-aspect- ratio wing-body combinations at transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Robert V. Doggett, A. Gerald Rainey, and Langley Research Center (page images at HathiTrust)
• An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics / (Washington D.C. : National Aeronautics and Space Administration, 1959), by Robert V. Doggett, Homer G. Morgan, A. Gerald Rainey, and Langley Research Center (page images at HathiTrust)
• Transonic and supersonic ejection release characteristics of six dynamically scaled external-store shapes from an 0.086-scale model of a current fighter airplane / (Washington D.C. : National Aeronautics and Space Administration, 1959), by William F. Hinson and Langley Research Center (page images at HathiTrust)
• The transonic aerodynamic characteristics of two variable-sweep airplane configurations capable of low-level supersonic attack / (Washington D.C. : National Aeronautics and Space Administration, 1960), by Ralph P. Bielat, William J. Alford, A. Warner Robins, and Langley Research Center (page images at HathiTrust)
• Numerical calculation of transonic flow about slender bodies of revolution / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971), by Frank R. Bailey, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theoretical and experimental engine-inlet flow fields for fighter forebodies / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Steven F. Yaros and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Aerodynamic design for improved maneuverability by use of three-dimensional transonic theory / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Michael J. Mann, James C. Ferris, Richard L. Campbell, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Transonic and supersonic Euler computations of vortex-dominated flow fields about a generic fighter / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by Aga M. Goodsell, John E. Melton, and Ames Research Center (page images at HathiTrust)
• Planform curvature effects on flutter characteristics of a wing with 56 ̊leading-edge sweep and panel aspect ratio of 1.14 / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by Donald F. Keller, Theresa L. Pinkerton, M. C. Sandford, and Langley Research Center (page images at HathiTrust)
• Wind tunnel investigation of vortex flows on F/A-18 configuration at subsonic through transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by Gary E. Erickson and Langley Research Center (page images at HathiTrust)
• Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by Elizabeth B. Plentovich, M. B. Tracy, and Julio Chu (page images at HathiTrust)
• The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : suction coefficient analysis / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by Cuyler W. Brooks, William D. Harvey, Charles D. Harris, and Langley Research Center (page images at HathiTrust)
• A comparative study of the nonuniqueness problem of the potential equation / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by M. D. Salas, R. E. Melnik, A. Jameson, and Langley Research Center (page images at HathiTrust)
• Aerodynamic design of the contoured wind-tunnel liner for the NASA supercritical, laminar-flow-control, swept-wing experiment / (Washington, D.C. : National Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Perry A. Newman, John B. Peterson, E. Clay Anderson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Fuselage and nozzle pressure distributions of a 1/12-scale f-15 propulsion model at transonic speeds [microform] : effect of fuselage modifications and nozzle variables / ([Washington, D.C.?] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1984), by Odis C. Pendergraft, George T. Carson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• CAS2D - FORTRAN program for nonrotating blade-to-blade, steady potential transonic cascade flows / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Djordje S. Dulikravich, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Jet exhaust and support interference effects on the transonic aerodynamic characteristics of a fighter model with two widely spaced engines / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by William B. Compton and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Three-dimensional cavity flow fields at subsonic and transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by E. B. Plentovich and Langley Research Center (page images at HathiTrust)
• Close-range photogrammetric measurement of static deflections for an aeroelastic superficial wing / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Thomas A. Byrdsong, M. C. Sandford, Richard R. Adams, and Langley Research Center (page images at HathiTrust)
• Transonic Navier-Stokes solutions of three-dimensional afterbody flows / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by William B. Compton and Langley Research Center (page images at HathiTrust)
• Transonic aerodynamic characteristics of a proposed assured crew return capability (ACRC) lifting-body configuration / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by George M. Ware and Langley Research Center (page images at HathiTrust)
• Theoretical estimation of the transonic aerodynamic characteristics of a supercritical-wing transport model with trailing-edge controls / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by James M. Luckring, Michael J. Mann, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Pierce L. Lawing, Charles L. Ladson, Jerry B. Adcock, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• High Reynolds number tests of a C141A aircraft semispan model to investigate shock-induced separation / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by W. T. Blackerby, J. F. Cahill, Ames Research Center, and Lockheed-Georgia Company (page images at HathiTrust)
• Transonic airfoil flowfield analysis using Cartesian coordinates / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Leland A. Carlson, Langley Research Center, and Texas A. and M. Research Foundation (page images at HathiTrust)
• Investigation of Northrop F-5A wing buffet intensity in transonic flight / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Chintsun Hwang, W. S. Pi, Ames Research Center, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Transonic performance of a Mach 2.65 auxiliary flow axisymmetric inlet / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Don M. Santman, United States National Aeronautics and Space Administration, Ames Research Center, and Inc Ellco Engineering (page images at HathiTrust)
• Feasibility of combining linear theory and impact theory methods for the analysis and design of high speed configurations / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Service ; Springfield, Va. : For sale by the National Technical Information Service, 1979), by D. Brooke, D. V. Vondrasek, Langley Research Center, McDonnell Douglas Corporation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Numerical computation of transonic flows by finite-element and finite-diffence methods / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. for sale by the National Technical Information Service, 1978), by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, M. M. Hafez, Langley Research Center, and inc Flow Research (page images at HathiTrust)
• Finite element analysis of transonic flows in cascades : importance of computational grids in improving accuracy and convergence / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Akin Ecer, Hasan U. Akay, IUPUI (Campus), United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
• Transonic pressure measurements and comparison of theory to experiment for three arrow-wing configurations : summary report / (Washington. D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Marjorie E. Manro, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Three-dimensional transonic potential flow about complex three-dimensional configurations / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Theodore A. Reyhner, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Boeing Commercial Airplane Company, and Langley Research Center (page images at HathiTrust)
• A direct-inverse method for transonic and separated flows about airfoils / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Leland A. Carlson, Langley Research Center, and Texas A & M University. Aerospace Engineering Dept (page images at HathiTrust)
• Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1988), by John Kuhlmann, Michael J. Cerney, Paul Liaw, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Method to predict external store carriage characteristics at transonic speeds / Bruce S. Rosen. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1988), by Bruce S. Rosen and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Analysis of transonic flow about lifting wing-body configurations / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Richard W. Barnwell and Langley Research Center (page images at HathiTrust)
• Effects of jet exhaust gas properties on exhaust simulation and afterbody drag / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by William B. Compton and Langley Research Center (page images at HathiTrust)
• A transonic investigation of base pressures associated with shallow three-dimensional rearward-facing steps / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1965]), by Thomas C. Kelly and Langley Research Center (page images at HathiTrust)
• Effect of nonlifting empennage surfaces on single-engine afterbody/nozzle drag at Mach numbers from 0.5 to 2.2 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Bobby L. Berrier and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Some anomalies observed in wind-tunnel tests of a blunt body at transonic and supersonic speeds / (Washington : National Aeronautics and Space Administration ; Springfield, Va. for sale by the National Technical Information Service, 1976), by Joseph D. Brooks, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• FORTRAN program for calculating transonic velocities on a blade-to-blade stream surface of a turbomachine / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1969), by Theodore Katsanis, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• FORTRAN program for calculating velocities and streamlines on a blade-to-blade stream surface of a tandem blade turbomachine / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, [1969]), by Theodore Katsanis, William D. McNally, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Evaluation of a technique for determining airplane aileron effectiveness and roll rate by using an aeroelastically scaled model / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Irving Abel, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An investigation of transonic flow fields surrounding hot and cold sonic jets / (Washington : National Aeronautics and Space Administration, [1961]), by George Lee and Ames Research Center (page images at HathiTrust)
• Experimental investigation at transonic speeds of pressure distributions over wedge and circular-arc airfoil sections and evaluation of perforated-wall interference / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Earl D. Knechtel and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Measurements of surface-pressure and wake-flow fluctations in the flow field of a Whitcomb supercritical airfoil / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Frederick W. Roos, Dennis W. Riddle, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A theory for base pressures in transonic and supersonic flow / (Urbana, Ill. : Mechanical Engineering Dept., Univ. of Illinois, 1955), by Helmut Hans Korst, M. E. Childs, R. H. Page, and University of Illinois (Urbana-Champaign campus). Engineering Experiment Station (page images at HathiTrust; US access only)
• Truncated cone in supersonic flight at zero angle of attack : surface pressure coefficients, drag coefficients, and shock front configurations / (Urbana, Ill. : Mechanical Engineering Dept., Engineering Experiment Station, University of Illinois, Jan. 1960), by W. L. Chow, C.C. Tsung, Helmut Hans Korst, and University of Illinois (Urbana-Champaign campus). Engineering Experiment Station (page images at HathiTrust; US access only)
• A theory for base pressures in transonic and supersonic flow / (Urbana, Ill. : Mechanical Engineering Dept., Univ. of Illinois, May 1962), by Helmut Hans Korst, M. E. Childs, R. H. Page, and University of Illinois (Urbana-Champaign campus). Engineering Experiment Station (page images at HathiTrust; US access only)
• Compressible two-dimensional jet mixing at constant pressure : tables of auxiliary functions for fully developed mixing profiles / (Urbana, Ill. : Mechanical Engineering Dept., University of Illinois, April 1955), by Helmut Hans Korst, M. E. Childs, R. H. Page, and University of Illinois (Urbana-Champaign campus). Engineering Experiment Station (page images at HathiTrust; US access only)
• On the range of applicability of the transonic area rule / (Washington, D.C. : NACA, 1954), by John R. Spreiter, United States. National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
• Linear aerodynamic loads on cone-cylinders at Mach numbers from 0.7 to 2.0 / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by Roger Lee Hamner and Alan D. Leff (page images at HathiTrust; US access only)
• Effects of leading-edge sweep on flutter characteristics of some delta-planform surfaces at a Mach number of 15.4 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1964), by Robert C. Goetz, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Transonic aerodynamic characteristics of several bodies having elliptical cross sections and various plan forms / (Washington : National Aeronautics and Space Administration, [1959]), by Robert A. Taylor and Ames Research Center (page images at HathiTrust)
• Dynamic response of hammerhead launch vehicles to transonic buffeting / (Washington, D.C. : National Aeronautics and Space Administration, 1963), by Henry A. Cole, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Effect of plug base contour on performance of a fully truncated plug nozzle with translating shroud / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Charles E. Mercer, Bobby L. Berrier, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Computation of the potential function of a compressible fluid near Mach number 1 / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Howard Tashjian, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Surface pressure distributions on 0.0628-scale models of proposed project fire space vehicles at Mach numbers from 0.25 to 4.63 / (Washington, D.C. : National Aeronautics and Space Administration, 1963), by Albin O. Pearson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• The effects of wing incidence on the aerodynamic loading characteristics of a sweptback wing-body combination at transonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Harold L. Robinson, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Fuselage and nozzle pressure distributions on a 1/12-scale F-15 propulsion model at transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by Odis C. Pendergraft, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• High speed aerodynamics and jet propulsion. (Princeton, N.J., Princeton University Press, 195?-) (page images at HathiTrust)
• Unsteady transonic flow. (New York, Pergamon Press, 1961), by Mårten Landahl (page images at HathiTrust)
• Computation of the transonic flow over a wedge with detached shock wave by the method of steepest descent /, by Joseph W. Fischbach, U.S. Army Ballistic Research Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Effects of overhang balance on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60 degree delta wing at transonic and supersonic speeds /, by Lawrence D. Guy, Langley Aeronautical Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Aerodynamic characteristics at transonic and supersonic speeds of a rocket-propelled airplane configuration having a diamond-plan-form wing aspect ration 3.08 and a low, swept horizontal tail /, by Alan B. Kehlet, Langley Aeronautical Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Loads on thin wings at transonic speeds /, by Don D. Davis, Gerald Hieser, Langley Aeronautical Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Loads on external stores at transonic and supersonic speeds /, by Lawrence D. Guy, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Investigation at transonic speeds of the hinge-moment characteristics of a 1/8-scale model of the X-1E aileron /, by William C. Moseley, Langley Aeronautical Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches /, by Charles F. Whitcomb, Harry T. Norton, Langley Aeronautical Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections /, by Jack F. Runckel, Edwin E.. Jr Lee, Langley Aeronautical Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Transonic wind-tunnel investigation of the effects of sweepback and thickness ratio on the wing loads of a wing-body combination of aspect ratio 4 and taper ratio 0.6 /, by Robert J. Platt, Joseph D. Brooks, Langley Aeronautical Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• A summary of information on support interference at transonic and supersonic speeds / (Washington, D.C. : NACA, 1954), by Eugene S. Love, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• A study of the flow over a 45À sweptback wing -fuselage combination at transonic Mach numbers / (Washington, D.C. : NACA, 1952), by Richard T. Whitcomb, Thomas C. Kelly, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Some examples of the applications of the transonic and supersonic area rules to the prediction of wave drag / (Washington, D.C. : NACA, 1957), by Robert L. Nelson, Clement J. Welsh, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Computation of unsteady transonic flows through rotating and stationary cascades. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by John I. Erdos, Lewis Research Center, and Advanced Technology Laboratories (page images at HathiTrust)
• Development of a multiple-parameter nonlinear perturbation procedure for transonic turbomachinery flows : preliminary application to design/optimization problems / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Stephen S. Stahara, John R. Spreiter, J. P. Elliott, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Laser anemometer measurements in a transonic axial-flow fan rotor / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by Anthony J. Strazisar and Lewis Research Center (page images at HathiTrust)
• Numerical computation of shock wave : turbulent boundary layer interaction in transonic flow over an axisymmetric curved hill / ([Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1989]), by S.-W. Kim and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Navier-Stokes analysis of transonic cascade flow ([Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]), by A. Arnone, Louis A. Povinelli, M. S. Liou, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Interference effects at transonic speeds of jets exhausting from the hull step of a model of a large, water-based airplane / (Washington [D.C.] : National Aeronautics and Space Administration, [1960]), by Beverly Z. Henry and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics of a 0.0667-scale model of the North American X-15 research airplane at transonic speeds / (Washington [D.C.] : National Aeronautics and Space Administration, [1959]), by Robert S. Osborne and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Observations on the flows past blunt bodies at transonic speeds / (Washington [D.C.] : National Aeronautics and Space Administration, [1960]), by Philip E. Everhart, Walter F. Lindsey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transonic flutter study of a 50.5 ̊cropped-delta wing with two rearward-mounted nacelles / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by M. C. Sandford, Irving Abel, Charles L. Ruhlin, and Langley Research Center (page images at HathiTrust)
• Transonic aerodynamic characteristics of a model of a proposed six-engine hull-type seaplane designed for supersonic flight / (Washington [D.C.] : National Aeronautics and Space Administration, [1960]), by Dewey E. Wornom and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Basic pressure measurements on a 0.0667-scale model of the North American X-15 research airplane at transonic speeds / (Washington [D.C.] : National Aeronautics and Space Administration, [1960]), by Robert S. Osborne, Virginia C. Stafford, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental study of the flutter of sails having a delta planform tested from a Mach number of 0.1 to a Mach number of 1.9 / (Washington [D.C.] : National Aeronautics and Space Administration, [1961]), by R. W. Hess, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A transonic wind-tunnel investigation of the static longitudinal and lateral aerodynamic characteristics of a proposed hypersonic glider with several booster configurations / (Washington [D.C.] : National Aeronautics and Space Administration, [1960]), by Ralph P. Bielat, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Extraction from flight data of longitudinal aerodynamic coefficients for F-8 aircraft with supercritical wing / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by James L. Williams, William T. Suit, and Langley Research Center (page images at HathiTrust)
• NASA supercritical airfoils : a matrix of family-related airfoils / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Charles D. Harris and Langley Research Center (page images at HathiTrust)
• High Reynolds number tests of a NASA SC(3)-0712(B) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by William G. Johnson, Otto Eichmann, Acquilla S. Hill, and Langley Research Center (page images at HathiTrust)
• Calculative techniques for transonic flows about certain classes of wing-body combinations / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Stephen S. Stahara, John R. Spreiter, Ames Research Center, and Nielsen Engineering & Research (page images at HathiTrust)
• A finite difference method for the solution of the transonic flow around harmonically oscillating wings / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by F. Edward Ehlers, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Development of a nonlinear unsteady transonic flow theory / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Stephen S. Stahara, John R. Spreiter, Langley Research Center, and Nielsen Engineering & Research (page images at HathiTrust)
• A study of the asymmetric transonic flow past a sharp leading edge / (Washington, DC : U.S. G.P.O., 1960), by Howard A. Stine, Alvin L. Lugn, Cleo B. Wagoner, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Theoretical pressure distributions on wings of finite span at zero incidence for mach numbers near 1 / (Washington, D.C. : U.S. G.P.O., 1961), by Alberta Y. Alksne, John R. Spreiter, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Numerical calculations of two-dimensional, unsteady transonic flows with circulation / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Richard M. Beam, Robert F. Warming, and Ames Research Center (page images at HathiTrust)
• Experimental investigation of a transonic compressor cascade and test results for four blade sections / (Washington [D.C.] : National Aeronautics and Space Administration, [1960]), by James C. Emery, Willard R. Westphal, James C. Dunavant, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Stability and control characteristics of a 0.0667-scale model of the final version of the North American X-15 research airplane (configuration 3) at transonic speeds / (Washington, [DC] : National Aeronautics and Space Administration, [1963]), by Robert S. Osborne, George M. Ware, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of tail size reductions on longitudinal aerodynamic characteristics of a three-surface F-15 model with nonaxisymmetric nozzles / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Mark C. Frassinelli, George T. Carson, and Langley Research Center (page images at HathiTrust)
• High Reynolds number test of a NACA 65₁-213, a = 0.5 airfoil at transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Kenneth P. Burdges, Gerald A. Pounds, James A. Blackwell, Langley Research Center, and Lockheed-Georgia Company (page images at HathiTrust)
• Some observations of the effects of radial distortions on performance of a transonic rotating blade row / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Donald M. Sandercock, Nelson L. Sanger, and Lewis Research Center (page images at HathiTrust)
• Pressure distributions from high Reynolds number tests of a NASA SC(3)-0712(B) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by William G. Johnson, Otto Eichmann, Acquilla S. Hill, and Langley Research Center (page images at HathiTrust)
• Drag of a supercritical body of revolution in free flight at transonic speeds and comparison with wind-tunnel data / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by J. W. Usry, John W. Wallace, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Dynamics of high-drag probe shapes at transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, 1971), by Robert I. Sammonds, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Wall-interference assessment and corrections for transonic NACA 0012 airfoil data from various wind tunnels / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by Lawrence L. Green, Perry A. Newman, and Langley Research Center (page images at HathiTrust)
• Relative efficiency and accuracy of two Navier-Stokes codes for simulating attached transonic flow over wings / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by Daryl L. Bonhaus, Stephen F. Wornom, and Langley Research Center (page images at HathiTrust)
• A method for the design of transonic flexible wings / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Leigh Ann Smith, Richard L. Campbell, and Langley Research Center (page images at HathiTrust)
• Prediction of effects of wing contour modifications on low-speed maximum lift and transonic performance for the EA-6B aircraft / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Dennis O. Allison, E. G. Waggoner, and Langley Research Center (page images at HathiTrust)
• Steady inviscid transonic flows over planar airfoils : a search for a simplified procedure / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by R. Magnus, H. Yoshihara, Ames Research Center, and General Dynamics Corporation. Convair Division (page images at HathiTrust)
• Aerodynamic characteristics of a swept-wing cruise missile at Mach numbers from 0.50 to 2.86 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by M. Leroy Spearman, Ida K. Collins, and Langley Research Center (page images at HathiTrust)
• Effects of increased leading-edge thickness on performance of a transonic rotor blade / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Lonnie Reid, Donald C. Urasek, and Lewis Research Center (page images at HathiTrust)
• Analytical method for predicting the pressure distribution about a nacelle at transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by J. S. Keith, Langley Research Center, and General Electric Company (page images at HathiTrust)
• High-speed flow past wings / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Helge Nørstrud, Langley Research Center, and Lockheed-Georgia Company (page images at HathiTrust)
• A study of the effects of Reynolds number and mach number on constant pressure coefficient jump for shock-induced trailing-edge separation / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Atlee M. Cunningham and Gregory S. Spragle (page images at HathiTrust)
• Hypersonic and transonic buzz measurements on the lower pitch flap of M2-F2 lifting entry configuration (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Robert W. Warner, Phillip R. Wilcox, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Computer program for definition of transonic axial flow compressor blade rows / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by James E. Crouse and Lewis Research Center (page images at HathiTrust)
• Transonic single-mode flutter and buffet of a low aspect ratio wing having a subsonic airfoil shape (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Larry L. Erickson, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Performance of a transonic compressor rotor with an aspect ratio of 6.5 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Lonnie Reid, Edward R. Tysl, and Lewis Research Center (page images at HathiTrust)
• Effect of blockage ratio on drag and pressure distributions for bodies of revolution at transonic speeds (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Lana M. Couch, Cuyler W. Brooks, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• High Reynolds number flows / (Washington : National Aeronautics and Space Administration ; [for sale by the National Technical Information Service, Springfield, Va.], 1971), by David A. Russell, United States National Aeronautics and Space Administration, and University of Washington (page images at HathiTrust)
• TAS--a transonic aircraft/store flow field prediction code / (Washington, D.C. : The Center : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by D. S. Thompson, General Dynamics Corporation. Fort Worth Division, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Ames Research Center (page images at HathiTrust)
• Calculation of unsteady transonic aerodynamics for oscillating wings with thickness / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1975), by S. Y. Ruo, J. G. Theisen, Langley Research Center, and Lockheed-Georgia Company (page images at HathiTrust)
• Some observations about the components of transonic fan noise from narrow-band spectral analysis / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Arthur V. Saule and Lewis Research Center (page images at HathiTrust)
• Wind-tunnel tests of modified cross, hemisflo, and disk-gap-band parachutes with emphasis in the transonic range / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by James T. Foughner, William C. Alexander, and Langley Research Center (page images at HathiTrust)
• Extraction from flight data of lateral aerodynamic coefficients for F-8 aircraft with supercritical wing / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by James L. Williams, William T. Suit, and Langley Research Center (page images at HathiTrust)
• Some effects of tip fins of wing flutter characteristics / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Robert C. Goetz, Robert V. Doggett, and Langley Research Center (page images at HathiTrust)
• Investigation of new radar-data-reduction techniques used to determine drag characteristics of a free-flight vehicle / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Gerard E. Woodbury, John W. Wallace, and Langley Research Center (page images at HathiTrust)
• An analysis method for two-dimensional transonic viscous flow / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Paul C. Bavitz and Langley Research Center (page images at HathiTrust)
• Calculation of the twist distribution of wings designed for cruise at transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Michael J. Mann and Langley Research Center (page images at HathiTrust)
• Experimental parametric studies of transonic T-tail flutter / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Charles L. Ruhlin, M. C. Sandford, and Langley Research Center (page images at HathiTrust)
• Performance of a 1.57-pressure-ratio transonic fan stage with a screen-induced 90 ̊circumferential inlet flow distribution / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1976), by Nelson L. Sanger and Lewis Research Center (page images at HathiTrust)
• Numerical calculation of transonic boattail flow / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Wen L. Chow, Bernhard H. Anderson, Lawrence J. Bober, and Lewis Research Center (page images at HathiTrust)
• Effect of nacelles on aerodynamic characteristics of an executive-jet model with simulated, partial-chord, laminar-flow-control wing glove [microform] / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Richard L. Campbell, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Effect of high rotor pressure-surface diffusion on performance of a transonic turbine / (Washington, D.C. : National Advisory Committee for Aeronautics, 1955), by James W. Miser, Daniel E. Monroe, Warner L. Stewart, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Effect of a reduction in stator solidity on performance of a transonic turbine / (Washington [D.C.] : National Advisory Committee for Aeronautics, [1956]), by James W. Miser, Robert Y. Wong, Warner L. Stewart, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Drag measurements at transonic speeds of two bodies of fineness ratio 9 with different locations of maximum body diameter / (Washington, D.C. : National Advisory Committee for Aeronautics, 1948), by Jim Rogers Thompson, Max C. Kurbjun, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Miscellaneous directional-stability data for several airplane-like configurations from rocket-model tests at transonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Paul E. Purser, Jesse L. Mitchell, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• A preliminary investigation of aerodynamic characteristics of small inclined air outlets at transonic Mach numbers / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by Paul E. Dewey, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Investigation at transonic speeds of a fixed divergent ejector installed in a single-engine fighter model / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by John M. Swihart, Charles E. Mercer, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Transonic longitudinal aerodynamic effects of sweeping up the rear of the fuselage of a rocket-propelled airplane model having no horizontal tail / (Washington, D.C. : National Advisory Committee for Aeronautics, 1955), by James H. Parks, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Effect of wing-mounted external stores on the lift and drag of the Douglas D-558-II research airplane at transonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Jack Nugent, Flight Research Center (U.S.), and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• An evaluation of two cooling-air ejectors in flight at transonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, [1954]), by L. Stewart Rolls, C. Dewey Havill, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Ames Research Center (page images at HathiTrust)
• Aerodynamic characteristics of a wing with quarter-chord line swept back 35©�, aspect ratio 6, taper ratio 0.6, and NACA 65A006 airfoil section. Transonic-bump method / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by William C. Sleeman, William D. Morrison, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Error in airspeed measurement due to static-pressure field ahead of an open-nose air-inlet model at transonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Thomas C. O'Bryan, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Measurements of fluctuating pressures on the wing of a sweptback wind-body combination in the Langley 16-foot transonic tunnel / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by Louis W. Habel, Donald R. Bowman, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Investigation of transonic flutter characteristics of a thin 10 degree sweptback wing having an aspect ratio of 4 and a taper ratio of 0.6 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by George W. Jones, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Two-dimensional transonic flow past airfoils / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Yung-Huai Kuo and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• An experimental investigation of transonic flow past two-dimensional wedge and circular-arc sections using a Mach-Zehnder interferometer / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Arthur E. Bryson and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• An investigation at transonic speeds of the effects of thickness ratio and of thickened root sections on the aerodynamic characteristics of wings with 47©� sweepback, aspect ratio 3.5, and taper ratio 0.2 in the slotted test section of the Langley 8-foot high-speed tunnel / (Washington, D.C. : National Advisory Committee for Aeronautics, [1951]), by Ralph P. Bielat, Domenic A. Coppolino, Daniel E. Harrison, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Numerical simulation and comparison of symmetrical/supercritical airfoils for the near tip region of a helicopter in forward flight / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by F. F. Badavi and Langley Research Center (page images at HathiTrust)
• A transonic investigation of the effects of semisubmerged-store cavities and of slots on the zero-lift drag of a body of revolution / (Washington, D.C. : National Advisory Committee for Aeronautics, [1957]), by George H. Holdaway, Elaine W. Hatfield, Minor R. Wallace, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Ames Research Center (page images at HathiTrust)
• The effects on propulsion-induced aerodynamic forces of vectoring a partial-span rectangular jet at Mach numbers from 0.40 to 1.20 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Francis J. Capone and Langley Research Center (page images at HathiTrust)
• Results of two free-fall experiments on flutter of thin unswept wings in the transonic speed range / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by WIlliam T. Lauten, Herbert C. Nelson, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• An experimental investigation of the effects of Mach number, stabilizer dihedral, and fin torsional stiffness on the transonic flutter characteristics of a tee-tail / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Norman S. Land, Annie G. Fox, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Similarity laws for transonic flow about wings of finite span / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by John R. Spreiter and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Transonic Symposium: Theory, Application, and Experiment / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989-), by Application Transonic Symposium: Theory, Jerome T. Foughner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Computation of shock-free transonic flows for airfoil design / (New York, New York : New York University, Courant Institute of Mathematical Sciences, 1969), by David G. Korn, U.S. Atomic Energy Commission, and Courant Institute of Mathematical Sciences (page images at HathiTrust)
• Transonic aeroelastic analysis of launch vehicle configurations / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1988), by João Luiz Filgueiras de Azevedo and Langley Research Center (page images at HathiTrust)
• Effect of canard location and size on canard-wing interference and aerodynamic-center shift related to maneuvering aircraft at transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Blair B. Gloss and Langley Research Center (page images at HathiTrust)
• On slender-body theory at transonic speeds / (Washington, D.C. : NACA, 1954), by Keith C. Harder, E. B. Klunker, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Influence of the body flow field on the zero-lift wave drag of wing-body combinations modified in accordance with the transonic area rule / (Washington, D.C. : National Advisory Committee for Aeronautics, [1956]), by William A. Page, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Ames Research Center (page images at HathiTrust)
• Investigation of two-stage air-cooled turbine suitable for flight at mach number of 2.5. (Washington, D.C. : National Advisory Committee for Aeronautics, 1956), by James W. Miser, Warner L. Stewart, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Results of two experiments on flutter of high-aspect-ratio swept wings in the transonic speed range / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by William T. Lauten, Burke R. O'Kelly, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• An experimental study of five annular air inlet configurations at subsonic and transonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by Carroll R. Bryan, Frank F. Fleming, Jospeh R. Milillo, Robert E. Pendley, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Application of transonic area rule to a sharp-lipped ducted nacelle / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Richard E. Walters, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• A flight investigation of the transonic area rule for a 52.5©� sweptback wind-body configuration at Mach numbers between 0.8 and 1.6 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Sherwood Hoffman, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• An investigation of the effects of a geometric twist on the aerodynamic loading characteristics of a 45©� sweptback wing-body configuration at transonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Claude V. Williams, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• An experimental study of a method of designing the sweptback-wing - fuselage juncture for reducing the drag at transonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1955), by Robert R. Howell, Albert L. Braslow, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• The development of an 8-inch by 8-inch slotted tunnel for Mach numbers up to 1.28 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1955), by B. H. Little, James M. Cubbage, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Flutter characteristics of swept wings at transonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1955), by Laurence K. Loftin, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Investigation at transonic speeds of aerodynamic characteristics of an unswept semielliptical air inlet in the root of a 45©� sweptback wing / (Washington, D.C. : National Advisory Committee for Aeronautics, 1955), by Gene J. Bingham, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Span loadings due to wing twist at transonic and supersonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Frederick C. Grant, John P. Mugler, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Transonic flutter investigation of two 50©� semispan modified-delta wings with tip ailerons / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by Robert J. Platt, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Investigation of fixed-geometry supersonic inlets with bypass ducts for matching turbojet-engine air-flow requirements over a range of transonic and supersonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by Abraham Leiss, Walter J. Kouyoumjian, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• An analysis of the pressure distribution measured on a body of revolution at transonic speeds in the slotted test section of the Langley 8-foot transonic tunnel / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Bruce B. Estabrooks, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Transonic longitudinal aerodynamic characteristics of a fighter-type airplane model with a low-aspect-ratio unswept wing and tee-tail / (Washington, D.C. : National Advisory Committee for Aeronautics, 1956), by Gerald Hieser, Charles F. Reid, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Transonic flow past a wedge profile with detached bow wave : general analytical method and final calculated results / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Walter G. Vincenti, Cleo B. Wagoner, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• On a solution of the nonlinear differential equation for transonic flow past a wave-shaped wall / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Carl Kaplan and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• On transonic flow past a wave-shaped wall / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Carl Kaplan and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effect of longitudinal wings position on the pressure characteristics at transonic speeds of a 45©� sweptback wing-fuselage model / (Washington [D.C.] : National Advisory Committee for Aeronautics, [1953]), by William Solomon, James W. Schmeer, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effects of fences, leading-edge chord-extensions, bound-layer ramps, and trailing-edge flaps on the longitudinal stability of a twisted and cambered 60©� sweptback-wing--indented-body configuration at transonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Thomas L. Fischetti, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• An experimental transonic investigation of a 45©� sweptback wing-body combination with several types of body indentation with theoretical comparisons included / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Melvin M. Carmel, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Characteristics of loads in rough air at transonic speeds of rocket-powered models of a canard and a conventional-tail configuration / (Washington [D.C.] : National Advisory Committee for Aeronautics, [1955]), by A. James Vitale and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Transonic investigation at lifting conditions of streamline contouring in the sweptback-wing-fuselage juncture in combination with the transonic area rule / (Washington, D.C. : National Advisory Committee for Aeronautics, 1956), by William E. Palmer, Albert L. Braslow, Robert R. Howell, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Effects of two leading-edge modifications on the aerodynamic characteristics of a thin low-aspect-ratio delta wing at transonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, [1956]), by John P. Mugler and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Steady loads due to jet interference on wings, tails, and fuselages at transonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, [1957]), by John M. Swihart, Norman L. Crabill, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• High Reynolds number research : a workshop / (Washington : Scientific and Technical Information Office, National Aeronautics and Space Administration ; Springfield, Va. : for sale by National Technical Information Service, 1977), by Va.)) Workshop on High Reynolds Number Research ((1st : : 1976 : : Hampton, Donald D. Baals, and Joint Institute for Advancement of Flight Sciences (page images at HathiTrust)
• Unsteady subsonic and transonic potential flow over helicopter rotor blades / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Morris P. Isom, Ames Research Center, and Polytechnic Institute of New York (page images at HathiTrust)
• Experiments in transonic flow, (Wright Field, Dayton, Ohio, Headquarters, Wright Patterson Air Force Base, 1948), by Jean G. Goppert, Joseph Flatt, and California Institute of Technology (page images at HathiTrust)

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