Showing 1 - 20 results of 23 for search '', query time: 0.40s Refine Results
  1. 1
    Comparison of two computer programs by predicting turbulent mixing of helium in a ducted supersonic airstream /
    by Pan, Y. S.
    Published 1978
    Government Document Book
  2. 2
    The development of a three-dimensional partially elliptic flow computer program for combustor research /
    by Pan, Y. S.
    Published 1978
    Government Document Book
  3. 3
    A modificiation to linearized theory for prediction of pressure loadings on lifting surfaces at high supersonic Mach numbers and large angles of attack /
    by Carlson, Harry W.
    Published 1979
    Government Document Book
  4. 4
    Aerodynamic characteristics of a fixed arrow-wing supersonic cruise aircraft at Mach numbers of 2.30, 2.70, and 2.95 /
    by Morris, Odell A.
    Published 1978
    Government Document Book
  5. 5
    An improved supersonic, three-dimensional, external, inviscid flow field code /
    by Marconi, Frank
    Published 1979
    Government Document Book
  6. 6
    Theoretical evaluation of high-speed aerodynamics for arrow-wing configurations /
    by Dollyhigh, Samuel M.
    Published 1979
    Government Document Book
  7. 7
    Fluctuating loads measured on an over-the-wing supersonic jet model /
    by Willis, Conrad M.
    Published 1979
    Government Document Book
  8. 8
    Progress in supersonic cruise aircraft technology /
    by Driver, Cornelius
    Published 1978
    Government Document Book
  9. 9
    Effects of roughness size on the position of boundary-layer transition and on the aerodynamic characteristics of a 55 ̊swept delta wing at supersonic speeds /
    by Stallings, Robert L.
    Published 1977
    Government Document Book
  10. 10
    Wind-tunnel investigation at supersonic speeds of a canard-controlled missile with fixed and free-rolling tail fins /
    by Blair, A. B.
    Published 1978
    Government Document Book
  11. 11
    Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach number 0.2 /
    by Penland, Jim A.
    Published 1978
    Government Document Book
  12. 12
    Effects of spanwise nozzle geometry and location on the longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds /
    by Leavitt, Laurence D.
    Published 1978
    Government Document Book
  13. 13
    Experimental aerodynamic characteristics at Mach numbers from 0.60 to 2.70 of two supersonic cruise fighter configurations /
    by Dollyhigh, Samuel M.
    Published 1979
    Government Document Book
  14. 14
    Bumblebee Program - aerodynamic data /
    by Barnes, G. A.
    Published 1979
    Government Document Book
  15. 15
    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
  16. 16
    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
  17. 17
    Calculation of three-dimensional, inviscid supersonic, steady flows /
    by Moretti, Gino
    Published 1982
    Government Document Book
  18. 18
    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
  19. 19
    Wind-tunnel/flight correlation study of aerodynamic characteristics of a large flexible supersonic cruise airplane (XB-70-1).
    Published 1979
    Government Document Book
  20. 20
    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
Search Tools: RSS Feed – Email Search