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Interference (Aerodynamics)

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• Aerodynamics

• Electromagnetic compatibility rationale report : conducted test requirements for electronic equipments in air transportation facilities / (Washington, D.C. : Dept. of Transportation, Federal Aviation Administration, Systems Research and Development Service ; Springfield, Va. : For sale by the National Technical Information Service, [1976]), by J. C. Toler, C. L. Espy, J. A. Woody, Georgia Institute of Technology. Engineering Experiment Station, and United States. Federal Aviation Administration. Systems Research and Development Service (page images at HathiTrust)
• Theoretical investigation of the aerodynamic interference induced by cruise and lift fans on transport-type aircraft / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by M. R. Mendenhall, Selden B. Spangler, Marnix F. E. Dillenius, United States National Aeronautics and Space Administration, Ames Research Center, and Nielsen Engineering & Research (page images at HathiTrust)
• Test sections for small theoretical wind-tunnel-boundary interference on V/STOL models / (Washington, D.C. : National Aeronautics and Space Administration, 1968), by Ray H. Wright, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of wing planform and canard location and geometry on the longitudinal aerodynamic characteristics of a close-coupled canard wing model at subsonic speeds / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Blair B. Gloss and Langley Research Center (page images at HathiTrust)
• Flight-test investigation of the aerodynamic characteristics and flow interference effects about the aft fuselage of the F111A airplane / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Norman V. Taillon and Flight Research Center (U.S.) (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)
• Theoretical study of the use of variable geometry in the design of minimal-correction V/STOL wind tunnels / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1969), by Harry H. Heyson, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Aerodynamic characteristics of a parasol-wing--body combination utilizing favorable lift interference at Mach numbers from 3.00 to 4.63 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1968), by Odell A. Morris, Robert J. Mack, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of fineness and closure ratios on boattail drag of circular-arc afterbody models with jet exhaust at Mach numbers up to 1.3 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by David E. Reubush and Langley Research Center (page images at HathiTrust)
• Interference heating from interactions of shock waves with turbulent boundary layers at Mach 6 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Charles B. Johnson, Louis G. Kaufman, and Langley Research Center (page images at HathiTrust)
• An experimental investigation of a highly underexpanded sonic jet ejecting from a flat plate into a subsonic crossflow (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Craig S. Shaw, Richard J. Margason, United States National Aeronautics and Space Administration, and Langley 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)
• The effect of wind-tunnel wall interference on the performance of a fan-in-wing VTOL model / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Harry H. Heyson 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)
• Experimental investigation of wind-tunnel interference on the downwash behind an airfoil / (Washington, D.C. : National Advisory Committee for Aeronautics, 1937), by Abe Silverstein, S. Katzoff, and Langley Aeronautical Laboratory (page images at HathiTrust)
• A numerical method of calculating the boundary-induced interference in slotted of perforated wind tunnels of rectangular cross section / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1971), by James D. Keller, Ray H. Wright, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Aerodynamics of airframe-engine integration of supersonic aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966), by Mark R. Nichols, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Wind-tunnel lift interference on sweptback wings in rectangular test sections with slotted side walls / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1970), by Ray H. Wright, James D. Keller, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Jet-wake effect of a high-bypass engine on wing-nacelle interference drag of a subsonic transport airplane, (Washington, National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by James C. Patterson and Stuart G. Flechner (page images at HathiTrust; US access only)
• Aerodynamic interference effects on half-cone bodies with thin wings at Mach 10.03 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151] , 1970), by James C. Townsend, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Support interference of wind tunnel models : a selective annotated bibliography / (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 Marie H. Tuttle, Pierce L. Lawing, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Low-speed upwash interference on a transport model in a rectangular slotted-wall wind tunnel / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Michael J. Mann and Langley Research Center (page images at HathiTrust)
• Effects of axisymmetric and normal air jet plumes and solid plume on cylindrical afterbody pressure distributions at Mach numbers from 1.65 to 2.50 / (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 Peter F. Covell, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Installation effects of long-duct pylon-mounted nacelles on a twin-jet transport model with swept supercritical wing / (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 Edwin E. Lee, Odis C. Pendergraft, and Langley Research Center (page images at HathiTrust)
• Effect of symmetrical vortex shedding on the longitudinal aerodynamic characteristics of wing-body-tail combinations / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by M. R. Mendenhall, Jack Norman Nielsen, Ames Research Center, and Nielsen Engineering & Research (page images at HathiTrust)
• Wind tunnel and analytical investigation of over-the-wing propulsion/air frame interferences for a short-haul aircraft at Mach numbers from 0.6 to 0.78 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by O. D. Wells, Douglas Aircraft Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A method for calculating the aerodynamic loading on wing-body combinations at small angles of attack in supersonic flow / (Washington, D.C. : National Aeronautics and Space Administration, 1971), by Charlie M. Jackson, Wallace C. Sawyer, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Interference heating on a swept cylinder in region of intersection with a wedge at Mach number 8 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1965]), by Dennis M. Bushnell and Langley Research Center (page images at HathiTrust)
• Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Raymond E. Mineck and Langley Research Center (page images at HathiTrust)
• Wind tunnel blockage and support interference effects on winged-body models 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], 1974), by Bernard J. Blaha and Lewis Research Center (page images at HathiTrust)
• Thermal design for areas of interference heating on actively cooled hypersonic aircraft / (Washington : National Aeronautics and Space Administration, Scientific and Technical Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by R. L. Herring, J. E. Stone, McDonnell Douglas Corporation, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Interference drag in a simulated wing-fuselage juncture / (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 L. Kubendran, J. Hubbartt, H. McMahon, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, 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)
• 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)
• 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)
• Wind-tunnel investigation of a VTOL jet-transport model with powered lift engines in pods at wing midspan or inboard / (Washington, DC : National Aeronautics and Space Administration, 1970), by Raymond D. Vogler, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Calculated wind-tunnel-boundary lift-interference factors for rectangular perforated test sections / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1970]), by Benferd L. Schilling, Ray H. Wright, and Langley Research Center (page images at HathiTrust)
• Induced interference effects on the aerodynamic characteristics of a 0.16-scale six-jet V / by Matthew M. Winston. (Washington : National Aeronautics and Space Administration : [For sale by the National Technical Information Service, Springfield, Va.], 1970), by Matthew M. Winston, United States National Aeronautics and Space Administration, and Langley Research Center (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)
• Wind-tunnel lift interference on sweptback wings in rectangular test sections with slotted top and bottom walls / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by Ray H. Wright and Raymond L. Barger (page images at HathiTrust; US access only)
• Flow-field measurements downstream of two protuberances on a flat plate submerged in a turbulent boundary layer at Mach 2.49 and 4.44 / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Lana M. Couch, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Forces and moments due to air jets exhausting parallel to large flat plates in a near vacuum / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Joseph J. Janos, Sherwood Hoffman, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Experimental investigation of the use of slotted test-section walls to reduce wall interference for high-lift-model testing / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Kalman J. Grunwald, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• The normal component of the induced velocity in the vicinity of a lifting rotor and some examples of its application / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by Walter Castles, Jacob Henri De Leeuw, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Experimental investigation of the effects of support interference on the drag of bodies of revolution at a Mach number of 1.5 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Edward W. Perkins and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Analysis of the effects of wing interference on the tail contributions to the rolling derivatives / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by William H. Michael 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)
• Interference effects and drag of struts on a monoplae wing / (Washington D.C. : National Advisory Committee for Aeronautics ;, 1931), by Kenneth E. Ward and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Report on the special field "interference" to the wind tunnel committee in February 1945 / (Washington, D.C. : National Advisory Commitee for Aeronautics ;, [1953]), by Hermann Schlichting and United States. National Advisory Commitee for Aeronautics (page images at HathiTrust)
• Wall interference in wind tunnels with slotted and porous boundaries at subsonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, [1953]), by Barrett S. Baldwin, Earl D. Knechtel, John B. Turner, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Ames Research Center (page images at HathiTrust)
• General theory of wave-drag reduction for combinations employing quasi-cylindrical bodies with an application to swept-wing and body combinations / (Washington, D.C. : National Advisory Committee for Aeronautics, [1955]), by Jack N. Nielsen, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Ames Research Center (page images at HathiTrust)
• Wind tunnel investigation of effect of yaw on lateral-stability characteristics. 4 - Symmetrically tapered wing with a circular fuselage having a wedge-shaped rear and a vertical tail / (Washington, D.C. : National Advisory Committee for Aeronautics, [1942]), by Isidore G. Recant, Arthur R. Wallace, Langley Aeronautical Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Interference drag, air drag : theoretical and practical data on aerodynamic drag /, by Sighard F. Hoerner and issuing agency United States. Army Air Forces. Air Matériel Command (page images at HathiTrust)
• Sting interference effects on the Modified Basic Finner Missile at Mach numbers 0.3 through 1.3 /, by Edward J. Marquart, sponsor Calspan Field Services, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Interference on a model afterbody from downstream support hardware at transonic Mach numbers /, by Earl A. Price, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• An investigation of sting interference effects on an oscillating cone in transonic flow /, by Frederick B. Cyran, J. P. Christopher, Inc. ARO, 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)
• Sting interference effects as determined by measurements of dynamic stability derivatives, surface pressure, and base pressure for Mach numbers 2 through 8 /, by Bob L. Uselton, Frederick B. Cyran, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Application of linearized transonic theory to tunnel blockage interference /, by C. F. Lo, United States. Air Force. Arnold Air Force Base. sponsor, United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body, and Inc. ARO (page images at HathiTrust)
• Aerodynamic interference between stores /, by F. Carroll Dougherty, University of Colorado Boulder. |b Department of Aerospace Engineering. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)

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