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Jet nozzles

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• Nozzles

• Exhaust nozzles

• A comparison of the noise produced by a small jet on a moving vehicle with that in a free jet / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Thomas D. Norum, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
• Performance of twin two-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Francis J. Capone, Donald L. Maiden, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Free jet feasibility study of a thermal acoustic shield concept for AST/VCE application : single stream nozzles / (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 R. K. Majjigi, General Electric Company. Aircraft Engine Business Group, and Lewis Research Center (page images at HathiTrust)
• Crossflow in two-dimensional asymmetric nozzles / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Daniel I. Sebacher, Louis P. Lee, and Langley Research Center (page images at HathiTrust)
• Aircraft ground tests and subscale model results of axial thrust loss caused by thrust vectoring using turning vanes / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Steven A. Johnson and Dryden Flight Research Facility (page images at HathiTrust)
• Computer program for calculating the flow field of supersonic ejector nozzles / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Bernhard H. Anderson and Lewis Research Center (page images at HathiTrust)
• Assessment of an analytical procedure for predicting supersonic ejector nozzle performance / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Bernhard H. Anderson and Lewis Research Center (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)
• Performance of an isolated two-dimensional variable-geometry wedge nozzle with translating shroud and collapsing wedge at speeds up to Mach 2.01 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Donald L. Maiden and Langley Research Center (page images at HathiTrust)
• Internal performance of two nozzles utilizing gimbal concepts for thrust vectoring / (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 Bobby L. Berrier, John G. Taylor, and Langley Research Center (page images at HathiTrust)
• Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes / (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 Robert J. Foley, Odis C. Pendergraft, and Langley Research Center (page images at HathiTrust)
• Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20 / (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 Francis J. Capone, Mary L. Mason, and Langley Research Center (page images at HathiTrust)
• Parametric experimental investigation of a scramjet nozzle at Mach 6 with freon and argon or air used for exhaust simulation / (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 James M. Cubbage, William J. Monta, and Langley Research Center (page images at HathiTrust)
• Transonic off-design performance of a fixed divergent ejector designed for a mach number of 2.0 / (Washington [D.C.] : National Aeronautics and Space Administration, [1959]), by Harry T. Norton, Charles E. Mercer, Marlowe D. Cassetti, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Jet effects on annular base pressure and temperature in a supersonic stream / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1962), by Milton A. Beheim, Richard A. Yeager, and John L. Klann (page images at HathiTrust)
• Comparison of measured and calculated velocity profiles of a laminar incompressible free jet at low Reynolds numbers / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by George C. Greene and Langley Research Center (page images at HathiTrust)
• Interference between exhaust system and afterbody of twin-engine fuselage configurations / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Jack F. Runckel and Langley Research Center (page images at HathiTrust)
• Analysis and testing of two-dimensional slot nozzle ejectors with variable area mixing sections / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1973), by Gerald B. Gilbert, Philip G. Hill, Ames Research Center, and Dynatech R/D Company (page images at HathiTrust)
• Jet effects on the drag of conical afterbodies at spersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by William B. Compton and Langley Research Center (page images at HathiTrust)
• Experimental investigation of an axisymmetric free jet with an initially uniform velocity profile (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Thomas L. Labus, Eugene P. Symons, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Effect of fineness ratio on boattail drag of circular-arc afterbodies having closure ratios of 0.50 with jet exhaust at Mach numbers up to 1.30 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by David E. Reubush, Jack F. Runckel, and Langley Research Center (page images at HathiTrust)
• Jet effects on annular base pressure and temperature in a supersonic stream / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1962), by Milton A. Beheim, Richard A. Yeager, and John L. Klann (page images at HathiTrust)
• Effects of nozzle interfairing modifications on longitudinal aerodynamic characteristics of a twin-jet, variable-wing-sweep fighter model / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by David E. Reubush, Charles E. Mercer, and Langley Research Center (page images at HathiTrust)
• Effects of vibrational nonequilibrium on the inviscid design of an axisymmetric nozzle for hypersonic flow / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by John Benjamin Anders and Langley Research Center (page images at HathiTrust)
• A finite-difference analysis of the nozzle starting process in an expansion tunnel / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by K. James Weilmuenster and Langley Research Center (page images at HathiTrust)
• Experimental and numerical investigation of boundary-layer development and transition on the walls of a Mach 5 nozzle / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by William D. Harvey, Julius E. Harris, Aubrey M. Cary, and Langley Research Center (page images at HathiTrust)
• Examination of high pressure water jets for use in rock tunnel excavation / (Oak Ridge, Tenn. : Oak Ridge National Laboratory ; Springfield, Va.: available from National Technical Information Service, 1970), by W C McClain, G A Cristy, and Oak Ridge National Laboratory (page images at HathiTrust)
• Experimental study of the effectiveness of cylindrical plume simulators for predicting jet-on boattail drag at Mach numberes up to 1.30 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by David E. Reubush and Lanlgely 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)
• Two-phase flow in turbines and reaction nozzles, ([Washington] National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., [1970]), by V. D. Venediktov (page images at HathiTrust; US access only)
• Splitting supersonic nozzle flow into separate jets by overexpansion into a multilobed divergent nozzle / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1972), by Ronald G. Huff, Donald E. Groesbeck, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Outflow of a jet of compressed air into moving air. ([Dayton, Headquarters, Air Materiel Command, Wright-Patterson Air Force Base, 1949]), by M. Schaefer (page images at HathiTrust)
• A static investigation of the thrust vectoring system of the F/A-18 high-alpha research vehicle / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Mary L. Mason, Scott C. Asbury, Francis J. Capone, and Langley Research Center (page images at HathiTrust)
• Effects of installation of F101 DFE exhaust nozzles on the afterbody-nozzle characteristics of the F-14 airplane / (Washington, D.C. : U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va., : For sale by the National Technical Information Service], 1982), by David E. Reubush, John R. Carlson, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Pressures measured in flight on the aft fuselage and external nozzle of a twin-jet fighter / (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 Jack Nugent and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers / (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 Odis C. Pendergraft, E. Ann Bare, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Aeropulsive characteristics at Mach numbers up to 2.2 of axisymmetric and nonaxisymmetric nozzles installed on an F-18 model / (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 Francis J. Capone, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Experimental investigation of two nonaxisymmetric wedge nozzles at free-stream Mach numbers up to 1.20 / (Washington, D.C. : National Aeronautics and Space Administation, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Mary L. Mason, William Kelly Abeyounis, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps / (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 Lawrence D. Leavitt, Linda S. Bangert, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (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)
• Effect of a trade between boattail angle and wedge size on the performance of a nonaxisymmetric wedge nozzle / (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 George T. Carson, James R. Burley, E. Ann Bare, and Langley Research Center (page images at HathiTrust)
• Static internal performance of a two-dimensional convergent-divergent nozzle with thrust vectoring / (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 E. Ann Bare, David E. Reubush, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (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)
• Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 / (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 George T. Carson, Milton Lamb, and Langley Research Center (page images at HathiTrust)
• Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring / (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 Bobby L. Berrier 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)
• 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)
• Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability / (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 Mary L. Mason, James R. Burley, and Langley Research Center (page images at HathiTrust)
• Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities / (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 Laurence D. Leavitt, James R. Burley, and Langley Research Center (page images at HathiTrust)
• Flight investigation of installation effects on a plug nozzle with a series of boattailed primary shrouds installed on an underwing nacelle / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Verlon L. Head and Lewis Research Center (page images at HathiTrust)
• Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface F-15 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], 1983), by E. Ann Bare, Odis C. Pendergraft, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Cold-flow performance of several variations of a ram-air-cooled plug nozzle for supersonic-cruise aircraft / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Douglas E. Harrington, David M. Straight, Stanley M. Nosek, and Lewis Research Center (page images at HathiTrust)
• Flow visualization and interpretation of visualization data for deflected thrust V/STOL nozzles ([Washington, D.C. : National Aeronautics and Space Administration, 1984]), by H. C. Kao, Albert L. Johns, Paul L. Burstadt, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Internal pressure distributions for a two-dimensional thrust-reversing nozzle operating at a free-stream mach number of zero / (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 Lawrence E. Putnam, Edward G. Strong, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Experimental and analytical investigation of a nonaxisymmetric and wedge nozzle at static conditions / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by George T. Carson, Mary L. Mason, 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)
• Flight investigation of installation effects on a wedge nozzle installed on an underwing nacelle / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Albert L. Johns and Lewis Research Center (page images at HathiTrust)
• Cold-flow acoustic evaluation of a small-scale, divergent, lobed nozzle for supersonic jet noise suppression / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Ronald G. Huff, Donald E. Groesbeck, and Lewis Research Center (page images at HathiTrust)
• Effect of a simulated engine jet blowing above an arrow wing at mach 2.0 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Barrett L. Shrout, Clyde Hayes, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• An experimental investigation of thrust vectoring two-dimensional covergent-divergent nozzles installed in a twin-engine fighter model at high angles of attack / (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 Francis J. Capone, Laurence D. Leavitt, Mary L. Mason, and Langley Research Center (page images at HathiTrust)
• Internal performance of a hybrid axisymmetric/nonaxisymmetric convergent-divergent nozzle / (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 John G. Taylor and Langley Research Center (page images at HathiTrust)
• Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability / (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 George T. Carson, Francis J. Capone, and Langley Research Center (page images at HathiTrust)
• A method for calculating a real-gas two-dimensional nozzle contour including the effects of gamma / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Charles B. Johnson, Lillian R. Boney, and Langley Research Center (page images at HathiTrust)
• Effect of jet exit vanes on flow pulsations in an open-jet wind 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 L. Sellers 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)
• Thrust performance of isolated 36-chute suppressor plug nozzles with and without ejectors at Mach numbers from 0 to 0.45 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Douglas E. Harrington, Stanley A. Skebe, James J. Schloemer, and Lewis Research Center (page images at HathiTrust)
• Modifications to the nozzle test chamber to extend nozzle static-test capability / (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 J. Wayne Keyes and Langley Research Center (page images at HathiTrust)
• Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance 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 Theodore R. Creel, Fang-Jenq Chen, Ivan E. Beckwith, and Langley Research Center (page images at HathiTrust)
• Operating characteristics of the multiple critical venturi system and secondary calibration nozzles used for weight-flow measurements in the Langley 16-foot transonic 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 Bobby L. Berrier, Linda S. Bangert, Laurence D. Leavitt, and Langley Research Center (page images at HathiTrust)
• Boundary-layer separation on isolated boattail nozzles / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by William Kelly Abeyounis, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Static performance of a cruciform nozzle with multiaxis thrust-vectoring and reverse-thrust capabilities / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by David J. Wing, Scott C. Asbury, and Langley Research Center (page images at HathiTrust)
• Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics / (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 Laurence D. Leavitt, E. Ann Bare, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Reduction of acoustic disturbances in the test section of supersonic wind tunnels by laminarizing their nozzle and test section wall boundary layers by means of suction / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by W. Pfenninger, J. Syberg, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Use of multiple discrete wall jets for delaying boundary layer separation / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1974]), by J. D. McLean, H. J. Herring, Lewis Research Center, and Princeton University (page images at HathiTrust)
• Static and wind tunnel near-field/far-field jet noise measurements from model scale single-flow baseline and suppressor nozzles : summary report / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Carl L. Jaeck and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An improved analytical model of the separation region on boattail nozzles at subsonic speeds / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Walter M. Presz, John D. Buteau, Ronald W. King, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Refinement and application of acoustic impulse technique to study nozzle transmission characteristics / (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 M. Salikuddin, Lewis Research Center, Lockheed-Georgia Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Viscous computations of cold air/air flow around scramjet nozzle afterbody / (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 Oktay Baysal, Walter C. Englelund, Old Dominion University. Dept. of Mechanical Engineering and Mechanics, and Langley Research Center (page images at HathiTrust)
• Flow analysis and design optimization methods for nozzle afterbody of a hypersonic vehicle / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Oktay Baysal, Langley Research Center, and Old Dominion University. Dept. of Mechanical Engineering and Mechanics (page images at HathiTrust)
• Effects of temperature on noise of bypass jets as measured in the Langley noise research facility / (Washington, D.C. : National Aeronautics and Space Administration, [1964]), by George T. Kantarges, Jimmy M. Cawthorn, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Charts for equilibrium flow properties of air in hypervelocity nozzles / (Washington : National Aeronautics and Space Administration, [1962]), by Leland H. Jorgensen, Geyle M. Baum, and Ames Research Center (page images at HathiTrust)
• Jet effects on cylindrical afterbodies housing sonic and supersonic nozzles which exhaust against a supersonic stream at angles of attack from 90 ̊to 180 ̊/ (Washington : National Aeronautics and Space Administration, [1962]), by Lovick O. Hayman, Russell W. McDearmon, and Langley Research Center (page images at HathiTrust)
• A study of equilibrium real-gas effects in hypersonic air nozzles, including charts of thermodynamic properties for equilibrium air / (Washington : National Aeronautics and Space Administration, [1960]), by Wayne D. Erickson, Helen S. Creekmore, and Langley Research Center (page images at HathiTrust)
• Experimental nozzle expansion and flow characteristics of potassium vapor / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1966]), by Louis J. Goldman, Stanley M. Nosek, and Lewis Research Center (page images at HathiTrust)
• Loads induced on a flat plate at a Mach number of 4.5 with a sonic or supersonic jet exhausting normal to the surface / (Washington : National Aeronautics and Space Administration, [1963]), by William Letko and Langley Research Center (page images at HathiTrust)
• Hot-flow tests of a series of 10-percent-scale turbofan forced mixing nozzles / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Verlon L. Head, William H. Gerstenmaier, Louis A. Povinelli, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Static internal performance of ventral and rear nozzle concepts for short-takeoff and vertical-landing aircraft / (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 Richard J. Re, George T. Carson, and Langley Research Center (page images at HathiTrust)
• Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles / (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 Mary L. Mason, Bobby L. Berrier, and Langley Research Center (page images at HathiTrust)
• Local stability analysis for a planar shock wave / (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 M. D. Salas and Langley Research Center (page images at HathiTrust)
• Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ̊/ (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 Laurence D. Leavitt and Langley Research Center (page images at HathiTrust)
• Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20 / (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 George T. Carson, Mary L. Mason, Francis J. Capone, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (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)
• Static internal performance of convergent single-expansion-ramp nozzles with various combinations of internal geometric parameters / (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 E. Ann Bare and Francis J. Capone (page images at HathiTrust)
• Acoustic, performance, and wake survey measurements of a lobed velocity-decayer nozzle installed on a quieted TF-34 turbofan engine / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Nick E. Samanich, Laurence J. Heidelberg, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Acoustic tests of a 15.2-centimeter-diameter potential flow convergent nozzle / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Allen M. Karchmer, Robert Friedman, Robert G. Dorsch, and Lewis Research Center (page images at HathiTrust)
• Modification of a three-dimensional supersonic nozzle analysis and comparison with experimental data / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by Allan R. Bishop, Bobby W. Sanders, and Lewis Research Center (page images at HathiTrust)
• Effect of several geometric parameters on the static internal performance of three nonaxisymmetric nozzle concepts / (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 Bobby L. Berrier, Richard J. Re, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Effect of thrust vectoring and wing maneuver devices on transonic aeropropulsive characteristics of a supersonic fighter aircraft / (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 Francis J. Capone, David E. Reubush, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap / (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 Richard J. Re, Laurence D. Leavitt, and Langley Research Center (page images at HathiTrust)
• Acoustic and aerodynamic performance investigation of inverted velocity profile connualar plug nozzles / P.R. Knott, J.T. Blozy, and P.S. Staid. (Washington, D.C. : National Aeronautic and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by P. R. Knott, P. S. Staid, J. T. Blozy, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles : theory / (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 P. D. Thomas, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles : part 2 - applications / (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 P. D. Thomas, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Experimental investigation of shock-cell noise reduction for single-stream nozzles in simulated flight / (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 K. Yamamoto, Lewis Research Center, and General Electric Company. Aircraft Engine Business Group (page images at HathiTrust)
• Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight / (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 B. A. Janardan, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and General Electric Company (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)
• Noncavitating and cavitating performance of several low area ratio water jet pumps having throat lengths of 3.54 diameters / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by Nelson L. Sanger, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Surface pressure distributions with a sonic jet normal to adjacent flat surfaces at Mach 2.92 to 6.4 / (Washington : National Aeronautics and Space Administration, [1961]), by Robert W. Cubbison, James J. Ward, Bernhard H. Anderson, and Lewis Research Center (page images at HathiTrust)
• Performance study of rotating gas jet generator for strong traveling transverse acoustic modes / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by Marcus F. Heidmann, Lewis Research Center, and United States National Aeronautics and Space Administration (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)
• Scramjet nozzle design and analysis as applied to a highly integrated hypersonic research airplane / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by William J. Small, P. J. Johnston, John P. Weidner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Static and wind-on tests of an upper-surface-blown jet-flap nozzle arrangement for use on the Quiet Clean Shore-haul Experimental Engine (QCSEE) / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Arthur E. Phelps, 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)
• Induced interference effects on a four-jet VTOL configuration with various wing planforms in the transition speed range / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by James H. Otis and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Measured and calculated transmission losses of sound waves through a helium layer [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Thomas D. Norum, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Effects of geometry and jet velocity on noise associated with an upper-surface-blowing model / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Lorenzo R. Clark, James C. Yu, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Noncavitating and cavitating performance of two low-area-ratio water jet pumps with throat lengths of 5.66 diameters / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by Nelson L. Sanger and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• 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)
• Effect of convergent ejector nozzles on the boattail drag of a 16©� conical afterbody at Mach number of 0.6 to 1.26 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by James M. Cubbage, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Effect of free-stream Mach number on gross-force and pumping characteristics of several ejectors / (Washington [D.C.] : National Advisory Committee for Aeronautics, [1955]), by Leonard E. Stitt, Alfred S. Valerino, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Preliminary investigation of a perforated axially symmetric nozzle for varying nozzle pressure ratios / (Washington, D.C. : National Advisory Committee for Aeronautics, [1953]), by Eli Reshotko, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Transient and steady-state performance of a single turbojet combustor with four different fuel nozzles / (Washington [D.C.] : National Advisory Committee for Aeronautics, 1955), by Richard J. McCafferty, Richard H. Donlon, 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)
• Forces and moments produced by air and helium jets exhausting parallel to a flat plate in a near vacuum / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by Joseph J. Janos, Sherwood Hoffman, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Rapid evaluation of propulsion system effects., by T. E. Hickcox, W. H. Ball, R. A. Atkins, issuing body United States. Air Force. Systems Command, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Boeing Aerospace Company (page images at HathiTrust)
• Interaction effects of side jets issuing from flat plates and cylinders alined with a supersonic stream /, by James L. Amick, Paul B. Hays, sponsor United States. Wright Air Development Division, United States. Air Force. Air Research and Development Command. issuing body, and sponsor University of Michigan (page images at HathiTrust)
• Investigation of carbon (graphite) base materials suitable for rocket and ram-jet applications /, by William D. Smiley, issuing body Wright Air Development Center, sponsor United States. Air Force. Air Research and Development Command, and sponsor Stanford Research Institute (page images at HathiTrust)
• Integrated airframe - nozzle performance for designing twin-engine fighters., by Edsel R. Glasgow, D. A. Tappeiner, R. Posthumus, R. D. Grennan, R. A. Fox, Leonard D. Miller, Don M. Santman, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lockheed-California Company (page images at HathiTrust)
• Evaluation of the twin nozzle/afterbody drag and nozzle internal performance computer deck with ESIT free jet data /, by Phillip C. Everling, Douglas L. Bowers, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Integrated airframe - nozzle performance for designing twin-engine fighters., by Edsel R. Glasgow, T. J. Jones, T. E. Charbonneau, Leonard D. Miller, Don M. Santman, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lockheed-California Company (page images at HathiTrust)
• Integrated airframe - nozzle performance for designing twin-engine fighters., by Edsel R. Glasgow, T. J. Jones, D. A. Tappeiner, T. E. Charbonneau, D. K. Hill, R. D. Grennan, R. A. Fox, D. A. Fox, Leonard D. Miller, Don M. Santman, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lockheed-California Company (page images at HathiTrust)
• Integrated airframe - nozzle performance for designing twin-engine fighters., by Edsel R. Glasgow, D. K. Hill, R. D. Grennan, R. A. Fox, Leonard D. Miller, Don M. Santman, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lockheed-California Company (page images at HathiTrust)
• Contributions to the theory of the spreading of a free jet issuing from a nozzle / (Washington, D.C. : NACA, 1951), by W. Szablewski and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Investigation of carbon (graphite) base materials suitable for rocket and ram-jet applications /, by William D. Smiley, issuing body Wright Air Development Center, sponsor United States. Air Force. Air Research and Development Command, and sponsor Stanford Research Institute (page images at HathiTrust)
• Integrated airframe - nozzle performance for designing twin-engine fighters., by Edsel R. Glasgow, T. J. Jones, T. E. Charbonneau, Leonard D. Miller, Don M. Santman, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lockheed-California Company (page images at HathiTrust)
• An investigaion of boattail geometry and Reynolds number effects on forebody and afterbody drag at transonic Mach numbers /, by A. V. Spratley, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• Computation of axisymmetric separated nozzle-afterbody flow /, by James L. Jacocks, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Towards high-Reynolds number quiet flow in hypersonic tunnels /, by Doyle D. Knight, Hadassah Naiman, sponsor Rutgers University. Department of Mechanical & Aerospace Engineering, and issuing body United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Experimental method for correcting nozzle afterbody drag for the effects of jet temperature /, by W. L. Peters, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Method for calculation of the one-dimensional nonequilibrium flow of a general gas mixture through a hypersonic nozzle /, by George Emanuel, Walter G. Vincenti, sponsor Stanford University. Department of Aeronautics and Astronautics, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• An investigation of F-16 nozzle-afterbody forces at transonic Mach numbers with emphasis on support system interference /, by Earl A. Price, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Inviscid and viscous hypersonic nozzle flow with finite rate chemical reactions /, by E. S. Levinsky, Jerome James Brainerd, sponsor General Dynamics Corporation. Astronautics Division, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Evaluation of various exhaust nozzles at free-stream Mach numbers from 0.6 to. 3.0 /, by Lawrence L. Galigher, Arnold Engineering Development Center. sponsor, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• A method for estimating jet entrainment effects on nozzle-afterbody drag /, by R. C. Bauer, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Exhaust plume temperature effects on nozzle afterbody performance over the transonic Mach number range /, by C. E. Robinson, M. Dean High, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Afterbody drag investigation of a twin-nozzle fighter-type model at Mach numbers from 0.6 to 1.5 /, by Earl A. Price, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Evaluation of Reynolds number and tunnel wall porosity effects on nozzle afterbody drag at transonic mach numbers /, by C. E. Robinson, Arnold Engineering Development Center. sponsor, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Evaluation of boattail geometry and exhaust plume temperature effects on nozzle afterbody drag at transonic Mach numbers /, by L. L. Galigher, R. C. Bauer, Steven F. Yaros, Arnold Engineering Development Center. sponsor, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Development and testing of a new optimum design code for hypersonic wind tunnel nozzles, including boundary layer, turbulence, and real gas effects /, by Ralph C. Tolle, Air Force Wright Aeronautical Laboratories. issuing body, and Air Force Flight Dynamics Laboratory (U.S.). sponsor (page images at HathiTrust)
• Determining operational states of turbojet engines with variable-area tail nozzle /, by Siegfried H. Hasinger and issuing agency United States. Army Air Forces. Air Matériel Command (page images at HathiTrust)

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