Showing 1 - 7 results of 7 for search 'Stivers, Louis S.', query time: 0.05s Refine Results
  1. 1
    The effectiveness at high subsonic Mach numbers of a 20-percent-chord plain traiiling-edge flap on the NACA 65-210 airfoil section /

    The effectiveness at high subsonic Mach numbers of a 20-percent-chord plain traiiling-edge flap on the NACA 65-210 airfoil section / by Stivers, Louis S.

    Published 1954
    Government Document Book
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  2. 2
    Effects of fixing boundary-layer transition for an unswept-wing model and an evaluation of porous tunnel-wall interference for Mach numbers from 0.60 to 1.40 /

    Effects of fixing boundary-layer transition for an unswept-wing model and an evaluation of porous tunnel-wall interference for Mach numbers from 0.60 to 1.40 / by Stivers, Louis S.

    Published 1958
    Government Document Book
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  3. 3
    Effects of subsonic Mach number on the forces and pressure distributions on four NACA 64A-series airfoil sections at angles of attack as high as 28 degrees /

    Effects of subsonic Mach number on the forces and pressure distributions on four NACA 64A-series airfoil sections at angles of attack as high as 28 degrees / by Stivers, Louis S.

    Published 1954
    Government Document Book
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  4. 4
    Aerodynamic characteristics of four NACA airfoil sections designed for helicopter rotor blades /

    Aerodynamic characteristics of four NACA airfoil sections designed for helicopter rotor blades / by Stivers, Louis S.

    Published 1946
    Government Document Book
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  5. 5
    Aerodynamic characteristics of the NACA 747A315 and 747A415 airfoils from tests in the NACA two-dimensional low-turbulence pressure tunnel /

    Aerodynamic characteristics of the NACA 747A315 and 747A415 airfoils from tests in the NACA two-dimensional low-turbulence pressure tunnel / by Von Doenhoff, Albert E.

    Published 1944
    Other Authors: “…Stivers, Louis S.…”
    Government Document Book
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  6. 6
    Summary of airfoil data /

    Summary of airfoil data / by Abbott, Ira H. A.

    Published 1945
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    Government Document Book
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  7. 7
    Low-speed test of five NACA 66-series airfoils having mean lines designed to give high critical Mach numbers /

    Low-speed test of five NACA 66-series airfoils having mean lines designed to give high critical Mach numbers / by Von Doenhoff, Albert E.

    Published 1947
    Other Authors: “…Stivers, Louis S.…”
    Government Document Book
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