Interference (Aerodynamics)See also what's at your library, or elsewhere.
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Filed under: Interference (Aerodynamics)- Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques (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)
- Wall-interference assessment and corrections for transonic NACA 0012 airfoil data from various wind tunnels (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by Lawrence L. Green, Perry A. Newman, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Edwin E. Lee, Odis C. Pendergraft, 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 (National Aeronautics and Space Administration ;, 1974), by Bernard J. Blaha and Lewis Research Center (page images at HathiTrust)
- Low-speed upwash interference on a transport model in a rectangular slotted-wall wind tunnel (National Aeronautics and Space Administration ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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)
- Theoretical investigation of the aerodynamic interference induced by cruise and lift fans on transport-type aircraft (National Aeronautics and Space Administration ;, 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)
- 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 (National Aeronautics and Space Administration ;, 1977), by O. D. Wells, Douglas Aircraft Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Thermal design for areas of interference heating on actively cooled hypersonic aircraft (National Aeronautics and Space Administration, Scientific and Technical Office ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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)
- Test sections for small theoretical wind-tunnel-boundary interference on V/STOL models (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)
- Theoretical study of the use of variable geometry in the design of minimal-correction V/STOL wind tunnels (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1969), by Harry H. Heyson, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Effects of jet exhaust gas properties on exhaust simulation and afterbody drag (National Aeronautics and Space Administration ;, 1975), by William B. Compton and Langley Research Center (page images at HathiTrust)
- Wind-tunnel lift interference on sweptback wings in rectangular test sections with slotted top and bottom walls (National Aeronautics and Space Administration, 1966), by Ray H. Wright and Raymond L. Barger (page images at HathiTrust)
- NASA TR R-379 (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)
- Effect of wing planform and canard location and geometry on the longitudinal aerodynamic characteristics of a close-coupled canard wing model at subsonic speeds (National Aeronautics and Space Administration ;, 1975), by Blair B. Gloss and Langley Research Center (page images at HathiTrust)
- NASA TN D-5147 (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)
- Surface pressure distributions with a sonic jet normal to adjacent flat surfaces at Mach 2.92 to 6.4 (National Aeronautics and Space Administration, 1961), by Robert W. Cubbison, James J. Ward, Bernhard H. Anderson, and Lewis Research Center (page images at HathiTrust)
- NASA TN D-5297 (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)
- Jet-wake effect of a high-bypass engine on wing-nacelle interference drag of a subsonic transport airplane (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)
- Effect of nonlifting empennage surfaces on single-engine afterbody/nozzle drag at Mach numbers from 0.5 to 2.2 (National Aeronautics and Space Administration ;, 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 (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)
- NASA TN D-5898 (National Aeronautics and Space Administration :, 1970), by James C. Townsend, Langley Research Center, and United States National Aeronautics and Space Administration (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 (National Aeronautics and Space Administration ;, 1968), by Odell A. Morris, Robert J. Mack, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-3390 (National Aeronautics and Space Administration :, 1966), by Mark R. Nichols, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Induced interference effects on the aerodynamic characteristics of a 0.16-scale six-jet V / by Matthew M. Winston. (National Aeronautics and Space Administration :, 1970), by Matthew M. Winston, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Interference heating from interactions of shock waves with turbulent boundary layers at Mach 6 (National Aeronautics and Space Administration ;, 1974), by Charles B. Johnson, Louis G. Kaufman, and Langley Research Center (page images at HathiTrust)
- A method for calculating the aerodynamic loading on wing-body combinations at small angles of attack in supersonic flow (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)
- An investigation of transonic flow fields surrounding hot and cold sonic jets (National Aeronautics and Space Administration, 1961), by George Lee and Ames Research Center (page images at HathiTrust)
- Interference heating on a swept cylinder in region of intersection with a wedge at Mach number 8 (National Aeronautics and Space Administration ;, 1965), by Dennis M. Bushnell 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 (National Aeronautics and Space Administration ;, 1974), by Norman V. Taillon and Flight Research Center (U.S.) (page images at HathiTrust)
- An experimental investigation of a highly underexpanded sonic jet ejecting from a flat plate into a subsonic crossflow (National Aeronautics and Space Administration ;, 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 (National Aeronautics and Space Administration ;, 1973), by Lana M. Couch, Cuyler W. Brooks, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- NASA TN D-6292 (National Aeronautics and Space Administration ;, 1971), by Kalman J. Grunwald, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- The effect of wind-tunnel wall interference on the performance of a fan-in-wing VTOL model (National Aeronautics and Space Administration ;, 1974), by Harry H. Heyson and Langley Research Center (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 (National Aeronautics and Space Administration ;, 1973), by David E. Reubush 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 (National Aeronautics and Space Administration ;, 1974), by Blair B. Gloss and Langley Research Center (page images at HathiTrust)
- Report on the special field "interference" to the wind tunnel committee in February 1945 (National Advisory Commitee for Aeronautics ;, 1953), by Hermann Schlichting and United States. National Advisory Commitee for Aeronautics (page images at HathiTrust)
- Conducted test requirements for electronic equipments in air transportation facilities (Dept. of Transportation, Federal Aviation Administration, Systems Research and Development 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)
- Wall interference in wind tunnels with slotted and porous boundaries at subsonic speeds (National Advisory Committee for Aeronautics, 1953), by Barrett S. Baldwin, Earl D. Knechtel, John B. Turner, United States National Advisory Committee for Aeronautics, 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 (National Advisory Committee for Aeronautics, 1955), by Jack N. Nielsen, United States National Advisory Committee for Aeronautics, and Ames Research Center (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 (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 (National Advisory Committee for Aeronautics, 1951), by William H. Michael and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- The normal component of the induced velocity in the vicinity of a lifting rotor and some examples of its application (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)
- Steady loads due to jet interference on wings, tails, and fuselages at transonic speeds (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 (National Advisory Committee for Aeronautics ;, 1931), by Kenneth E. Ward and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- NACA Wartime Reports. Series L. (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)
- Investigation of wind-tunnel interference on the downwash behind an airfoil. (National Advisory Committee for Aeronautics, 1937), by Abe Silverstein, S. Katzoff, and Langley Aeronautical Laboratory (page images at HathiTrust)
- Sting interference effects on the Modified Basic Finner Missile at Mach numbers 0.3 through 1.3 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1982., 1982), by Edward J. Marquart, Calspan Field Services, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
- Application of linearized transonic theory to tunnel blockage interference (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1974., 1974), by C. F. Lo, United States. Air Force. Arnold Air Force Base, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
- Interference on a model afterbody from downstream support hardware at transonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), by Earl A. Price, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
- An investigation of sting interference effects on an oscillating cone in transonic flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), by Frederick B. Cyran, J. P. Christopher, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
- An investigation of F-16 nozzle-afterbody forces at transonic Mach numbers with emphasis on support system interference (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), by Earl A. Price, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (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 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), by Bob L. Uselton, Frederick B. Cyran, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
- Interference drag, air drag : theoretical and practical data on aerodynamic drag (Wright-Patterson Air Force Base, Dayton, Ohio : Central Air Documents Office (Army-Navy-Air Force), 1950., 1950), by Sighard F. Hoerner and United States. Army Air Forces. Air Matériel Command (page images at HathiTrust)
- Aerodynamic interference between stores (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1992., 1992), by F. Carroll Dougherty, University of Colorado Boulder. |b Department of Aerospace Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
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