Showing 121 - 140 results of 254 for search '', query time: 0.18s Refine Results
  1. 121
    Prediction of vortex shedding from circular and noncircular bodies in supersonic flow /
    by Mendenhall, M. R.
    Published 1984
    Government Document Book
  2. 122
    Correlations of supersonic boundary-layer transition on cones including effects of large axial variations in wind-tunnel noise /
    by Chen, Fang-Jenq
    Published 1984
    Government Document Book
  3. 123
    An experimental investigation of nacelle-pylon installation on an unswept wing at subsonic and transonic speeds /
    by Carlson, John R.
    Published 1984
    Government Document Book
  4. 124
    Body and canard effects on an attached-flow maneuver wing at Mach 1.62 /
    by Pittman, Jimmy L.
    Published 1984
    Government Document Book
  5. 125
    Theoretical and experimental engine-inlet flow fields for fighter forebodies /
    by Yaros, Steven F.
    Published 1984
    Government Document Book
  6. 126
    Study of supersonic wings employing the attainable leading-edge thrust concept /
    Government Document Book
  7. 127
    The wedge hot-film anemometer in supersonic flow /
    by Seiner, John M.
    Published 1983
    Government Document Book
  8. 128
    Low-speed aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wing /
    by Coe, Paul L.
    Published 1983
    Government Document Book
  9. 129
    Investigation of flow characteristics over missle bodies at supersonic speeds /
    by Barger, Raymond L.
    Published 1979
    Government Document Book
  10. 130
    Interference effects of aft reaction-control yaw jets on the aerodynamic characteristics of a space shuttle orbiter model at supersonic speeds /
    by Covell, Peter F.
    Published 1983
    Government Document Book
  11. 131
    A finite difference solution for the propagation of sound in near sonic flows /
    by Hariharan, S. I.
    Published 1983
    Government Document Book
  12. 132
    User's guide for a computer program for calculating the zero-lift wave drag of complex aircraft configurations /
    by Craidon, Charlotte B.
    Published 1983
    Government Document Book
  13. 133
    Aerodynamic characteristics of a Sparrow III missile model in the flow field of a generalized parent body at Mach 2.86 /
    by Stallings, Robert L.
    Published 1981
    Government Document Book
  14. 134
    The NCOREL computer program for 3D nonlinear supersonic potential flow computations /
    by Siclari, Michael J.
    Published 1983
    Government Document Book
  15. 135
    A wing concept for supersonic maneuvering /
    Government Document Book
  16. 136
    Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept /
    by Wood, Richard M.
    Published 1983
    Government Document Book
  17. 137
    Experimental investigation of leading-edge thrust at supersonic speeds /
    by Wood, Richard M.
    Published 1983
    Government Document Book
  18. 138
    Wing planform effects at supersonic speeds for an advanced fighter configuration /
    by Wood, Richard M.
    Published 1984
    Government Document Book
  19. 139
    Supersonic nonlinear potential flow analysis : interim report /
    by Siclari, Michael J.
    Published 1984
    Government Document Book
  20. 140
    PAN AIR, a computer program for predicting subsonic or supersonic linear potential flows about arbitrary configurations using a higher order panel method.
    Published 1981
    Government Document Book
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