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  1. 1
    Preliminary performance estimates of an oblique, all-wing, remotely piloted vehicle for air-to-air combat /

    Preliminary performance estimates of an oblique, all-wing, remotely piloted vehicle for air-to-air combat / by Nelms, Walter P.

    Published 1974
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  2. 2
    Study of inertial navigation errors during reentry to the earth's atmosphere /

    Study of inertial navigation errors during reentry to the earth's atmosphere / by Hansen, Q. Marion

    Published 1963
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  3. 3
    Motion and heating during atmosphere reentry of space vehicles /

    Motion and heating during atmosphere reentry of space vehicles / by Wong, Thomas J.

    Published 1960
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  4. 4
    Analytic and experimental performance of two isentropic mixed compression axisymmetric inlets at Mach numbers 0.8 to 2.65 /

    Analytic and experimental performance of two isentropic mixed compression axisymmetric inlets at Mach numbers 0.8 to 2.65 / by Smeltzer, Donald B.

    Published 1973
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  5. 5
    Experimental investigation of stability and stall flutter of a free-floating wing V/STOL model /

    Experimental investigation of stability and stall flutter of a free-floating wing V/STOL model / by Ormiston, Robert A.

    Published 1972
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  6. 6
    Extrapolation of sonic boom pressure signatures by the waveform parameter method /

    Extrapolation of sonic boom pressure signatures by the waveform parameter method / by Thomas, Charles L.

    Published 1972
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  7. 7
    Safe atmosphere entry of an isotope heat source with a single stable trim attitude at hypersonic speeds /

    Safe atmosphere entry of an isotope heat source with a single stable trim attitude at hypersonic speeds / by Levy, Lionel L.

    Published 1972
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  8. 8
    Takeoff certification considerations for large subsonic and supersonic transport airplanes using the Ames Flight Simulator for Advanced Aircraft /

    Takeoff certification considerations for large subsonic and supersonic transport airplanes using the Ames Flight Simulator for Advanced Aircraft /

    Published 1973
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  9. 9
    The application of space program fire-retardant technology to housing /

    The application of space program fire-retardant technology to housing / by Riccitiello, S. R.

    Published 1973
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  10. 10
    Leading-edge serrations which reduce the noise of low-speed rotors /

    Leading-edge serrations which reduce the noise of low-speed rotors / by Soderman, Paul T.

    Published 1973
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  11. 11
    Experimental investigation of a large-scale, two-dimensional, mixed-compression inlet system : internal performance and drag at transonic conditions, M[infinity]=0.6 to 1.28 / by Norman D. Wong and Warren E. Anderson.

    Experimental investigation of a large-scale, two-dimensional, mixed-compression inlet system : internal performance and drag at transonic conditions, M[infinity]=0.6 to 1.28 / by N... by Wong, Norman D.

    Published 1973
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  12. 12
    Analytical design of sensors for measuring atmospheric temperature during terminal phase of planetary entry /

    Analytical design of sensors for measuring atmospheric temperature during terminal phase of planetary entry / by Millard, John P.

    Published 1972
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  13. 13
    A preliminary investigation of projectile shape effects in hypervelocity impact of a double-sheet structure /

    A preliminary investigation of projectile shape effects in hypervelocity impact of a double-sheet structure / by Morrison, Robert H.

    Published 1972
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  14. 14
    Vacuum ultraviolet line radiation measurements of a shock-heated nitrogen plasma /

    Vacuum ultraviolet line radiation measurements of a shock-heated nitrogen plasma / by McClenahan, James O.

    Published 1972
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  15. 15
    Low speed aerodynamic characteristics of a large-scale model with a thin, highly swept, 2.67 aspect ratio wing having a cranked leading edge /

    Low speed aerodynamic characteristics of a large-scale model with a thin, highly swept, 2.67 aspect ratio wing having a cranked leading edge / by Giulianetti, Demo J.

    Published 1972
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  16. 16
    A method for calculating laminar viscous, compressible flows with small pressure gradients /

    A method for calculating laminar viscous, compressible flows with small pressure gradients / by Martin, E. Dale

    Published 1972
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  17. 17
    Prediction of static aerodynamic characteristics for space-shuttle-like and other bodies at angles of attack from 0̊ to 180̊ /

    Prediction of static aerodynamic characteristics for space-shuttle-like and other bodies at angles of attack from 0̊ to 180̊ / by Jorgensen, Leland H.

    Published 1973
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  18. 18
    Investigation, at inlet locations, of fuselage flow fields at transonic and supersonic speeds /

    Investigation, at inlet locations, of fuselage flow fields at transonic and supersonic speeds / by King, Lyndell S.

    Published 1973
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  19. 19
    The structure of an atmosphere from on-board measurements of pressure, temperature, and acceleration /

    The structure of an atmosphere from on-board measurements of pressure, temperature, and acceleration /

    Published 1967
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  20. 20
    Analog study of the longitudinal response of a swept-wing transport airplane to wind shear and sustained gusts during landing approach /

    Analog study of the longitudinal response of a swept-wing transport airplane to wind shear and sustained gusts during landing approach / by Snyder, C. Thomas

    Published 1968
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