Showing 81 - 100 results of 254 for search '', query time: 0.32s Refine Results
  1. 81
    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
  2. 82
    An improved supersonic, three-dimensional, external, inviscid flow field code /
    by Marconi, Frank
    Published 1979
    Government Document Book
  3. 83
    Theoretical evaluation of high-speed aerodynamics for arrow-wing configurations /
    by Dollyhigh, Samuel M.
    Published 1979
    Government Document Book
  4. 84
    Fluctuating loads measured on an over-the-wing supersonic jet model /
    by Willis, Conrad M.
    Published 1979
    Government Document Book
  5. 85
    Progress in supersonic cruise aircraft technology /
    by Driver, Cornelius
    Published 1978
    Government Document Book
  6. 86
    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
  7. 87
    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
  8. 88
    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
  9. 89
    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
  10. 90
    Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects - program documentation and test case /
    by Biringen, Sedat
    Published 1981
    Government Document Book
  11. 91
    A study of the sonic-boom characteristics of a blunt body at a Mach number of 6 /
    by Ashby, George C.
    Published 1980
    Government Document Book
  12. 92
    Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds /
    by Leavitt, Laurence D.
    Published 1979
    Government Document Book
  13. 93
    Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft /
    by Berrier, Bobby L.
    Published 1980
    Government Document Book
  14. 94
    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
  15. 95
    Bumblebee Program - aerodynamic data /
    by Barnes, G. A.
    Published 1979
    Government Document Book
  16. 96
    Pressure data for four analytically defined arrow wings in supersonic flow /
    Government Document Book
  17. 97
    Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds /
    by Carlson, Harry W.
    Published 1980
    Government Document Book
  18. 98
    Mechanical property characterization of Borsic®/aluminum laminates at room and elevated temperatures /
    by McWithey, Robert R.
    Published 1980
    Government Document Book
  19. 99
    Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 /
    by Pittman, Jimmy L.
    Published 1980
    Government Document Book
  20. 100
    Supersonic stability and control characteristics of a cruciform missile model with delta wings and aft tail fin controls /
    by Corlett, William A.
    Published 1979
    Government Document Book
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