Showing 101 - 120 results of 254 for search '', query time: 0.15s Refine Results
  1. 101
    A System for aerodynamic design and analysis of supersonic aircraft.
    Published 1980
    Government Document Book
  2. 102
    Surface pressure data on a series of analytic forebodies at Mach numbers from 1.70 to 4.50 and combined angles of attack and sideslip /
    Published 1979
    Government Document Book
  3. 103
    RAXJET : a computer program for predicting transonic, axisymmetric flow over nozzle afterbodies with supersonic jet exhausts /
    by Wilmoth, Richard G.
    Published 1982
    Government Document Book
  4. 104
    Longitudinal aerodynamic characteristics of an elliptical body with a horizontal tail at mach numbers 2.3 to 4.63 /
    by Shrout, Barrett L.
    Published 1982
    Government Document Book
  5. 105
    Surface pressure data on a series of conical forebodies at mach numbers from 1.70 to 4.50 and combined angles of attack and sideslip /
    Published 1979
    Government Document Book
  6. 106
    Some observations on a new numerical method for solving the Navier-Stokes equations /
    by Kumar, Ajay
    Published 1981
    Government Document Book
  7. 107
    Calculation of three-dimensional, inviscid supersonic, steady flows /
    by Moretti, Gino
    Published 1982
    Government Document Book
  8. 108
    Pressure and force data for a flat wing and a warped conical wing having a shockless recompression at Mach 1.62 /
    Published 1981
    Government Document Book
  9. 109
    Wing-alone aerodynamic characteristics for high angles of attack at supersonic speeds /
    by Stallings, Robert L.
    Published 1981
    Government Document Book
  10. 110
    Aerodynamic test and analysis of a turbojet-boosted launch vehicle concept (spacejet) over a Mach number range of 1.50 to 2.86 /
    by Riebe, Gregory D.
    Published 1981
    Government Document Book
  11. 111
    Surface pressure data for a supersonic-cruise airplane configuration at mach numbers of 2.30, 2.96, and 3.30 /
    by Shrout, Barrett L.
    Published 1979
    Government Document Book
  12. 112
    Effects of cortex flaps on the low-speed aerodynamic characteristics of an arrow wing /
    by Yip, Long P.
    Published 1981
    Government Document Book
  13. 113
    Supersonic wings with significant leading-edge thrust at cruise /
    by Robins, A. Warner
    Published 1982
    Government Document Book
  14. 114
    Development of the triplet singularity for the analysis of wings and bodies in supersonic flow /
    by Woodward, F. A.
    Published 1981
    Government Document Book
  15. 115
    Wind-tunnel/flight correlation study of aerodynamic characteristics of a large flexible supersonic cruise airplane (XB-70-1).
    Published 1979
    Government Document Book
  16. 116
    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
  17. 117
    Numerical simulation of steady supersonic viscous flow /
    by Schiff, Lewis B.
    Published 1981
    Government Document Book
  18. 118
    Steady and nonsteady supersonic turbulent afterbody flow /
    by Yoshikawa, Kenneth K.
    Published 1981
    Government Document Book
  19. 119
    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
  20. 120
    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
Search Tools: RSS Feed – Email Search