Showing 41 - 60 results of 127 for search '', query time: 0.16s Refine Results
  1. 41
    Development of the triplet singularity for the analysis of wings and bodies in supersonic flow /
    by Woodward, F. A.
    Published 1981
    Government Document Book
  2. 42
    Wind-tunnel/flight correlation study of aerodynamic characteristics of a large flexible supersonic cruise airplane (XB-70-1).
    Published 1979
    Government Document Book
  3. 43
    Velocity field of a round jet in a cross flow for various jet injection angles and velocity ratios /
    by Fearn, Richard L.
    Published 1979
    Government Document Book
  4. 44
    Numerical simulation of steady supersonic viscous flow /
    by Schiff, Lewis B.
    Published 1981
    Government Document Book
  5. 45
    Steady and nonsteady supersonic turbulent afterbody flow /
    by Yoshikawa, Kenneth K.
    Published 1981
    Government Document Book
  6. 46
    Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements /
    by Lamb, Milton
    Published 1981
    Government Document Book
  7. 47
    Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers /
    by Blair, A. B.
    Published 1983
    Government Document Book
  8. 48
    Prediction of vortex shedding from circular and noncircular bodies in supersonic flow /
    by Mendenhall, M. R.
    Published 1984
    Government Document Book
  9. 49
    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
  10. 50
    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
  11. 51
    Body and canard effects on an attached-flow maneuver wing at Mach 1.62 /
    by Pittman, Jimmy L.
    Published 1984
    Government Document Book
  12. 52
    Theoretical and experimental engine-inlet flow fields for fighter forebodies /
    by Yaros, Steven F.
    Published 1984
    Government Document Book
  13. 53
    Study of supersonic wings employing the attainable leading-edge thrust concept /
    Government Document Book
  14. 54
    The wedge hot-film anemometer in supersonic flow /
    by Seiner, John M.
    Published 1983
    Government Document Book
  15. 55
    Low-speed aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wing /
    by Coe, Paul L.
    Published 1983
    Government Document Book
  16. 56
    Investigation of flow characteristics over missle bodies at supersonic speeds /
    by Barger, Raymond L.
    Published 1979
    Government Document Book
  17. 57
    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
  18. 58
    A finite difference solution for the propagation of sound in near sonic flows /
    by Hariharan, S. I.
    Published 1983
    Government Document Book
  19. 59
    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
  20. 60
    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
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