Books by David E. Reubush:
Books in the extended shelves:
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Reubush, David E.: 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 (National Aeronautics and Space Administration ;, 1973), also by Jack F. Runckel and Langley Research Center (page images at HathiTrust)- Reubush, David E.: Effect of Reynolds number on the subsonic boattail drag of several wing-body configurations (U.S. National Aeronautics and Space Administration ;, 1976), also by United States National Aeronautics and Space Administration and Langley Research Center (page images at HathiTrust)
- Reubush, David E.: Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration (National Aeronautics and Space Administrat ion, Scientific and Technical Information Branch ;, 1979), also by Richard J. Re, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Reubush, David E.: Effect of thrust vectoring and wing maneuver devices on transonic aeropropulsive characteristics of a supersonic fighter aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Francis J. Capone and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Reubush, David E.: Effects of afterbody boattail design and empennage arrangement on aeropropulsive characteristics of a twin-engine fighter model at transonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Linda S. Bangert, Laurence D. Leavitt, and Langley Research Center (page images at HathiTrust)
- Reubush, David E.: 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), also by Langley Research Center (page images at HathiTrust)
- Reubush, David E.: Effects of installation of F101 DFE exhaust nozzles on the afterbody-nozzle characteristics of the F-14 airplane (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by John R. Carlson, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Reubush, David E.: Effects of nozzle interfairing modifications on longitudinal aerodynamic characteristics of a twin-jet, variable-wing-sweep fighter model (National Aeronautics and Space Administration ;, 1975), also by Charles E. Mercer and Langley Research Center (page images at HathiTrust)
- Reubush, David E.: Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), also by Bobby L. Berrier and Langley Research Center (page images at HathiTrust)
- Reubush, David E.: Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Francis J. Capone and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Reubush, David E.: Exhaust-nozzle characteristics for a twin-jet variable-wing-sweep fighter airplane model at Mach numbers to 2.2 (National Aeronautics and Space Administration ;, 1974), also by Charles E. Mercer and Langley Research Center (page images at HathiTrust)
- Reubush, David E.: An experimental and analytical investigation of the effect on isolated boattail drag of varying Reynolds number up to 130 x 106 (National Aeronautics and Space Administration ;, 1976), also by Lawrence E. Putnam, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Reubush, David E.: An experimental and theoretical investigation of the effect of nonmetric over-the-wing nacelles on wing-body aerodynamics (National Aeronautics and Space Administration ;, 1979), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Reubush, David E.: Experimental investigation to validate use of cryogenic temperatures to achieve high Reynolds numbers in boattail pressure testing (U.S. National Aeronautics and Space Administration ;, 1976), also by United States National Aeronautics and Space Administration and Langley Research Center (page images at HathiTrust)
- Reubush, David E.: Experimental study of the effectiveness of cylindrical plume simulators for predicting jet-on boattail drag at Mach numberes up to 1.30 (National Aeronautics and Space Administration ;, 1974), also by Lanlgely Research Center (page images at HathiTrust)
- Reubush, David E.: Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by E. Ann Bare, Raymond C. Haddad, and Langley Research Center (page images at HathiTrust)
- Reubush, David E.: Investigation of a supersonic cruise fighter model flow field (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by E. Ann Bare and Langley Research Center (page images at HathiTrust)
- Reubush, David E.: Investigation of very low blockage ratio boattail models in the Langley 16-foot transonic tunnel (National Aeronautics and Space Administration ;, 1976), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
- Reubush, David E.: Static internal performance of a two-dimensional convergent-divergent nozzle with thrust vectoring (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by E. Ann Bare and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
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