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  1. 1
    The effects of amount and type of camber on the variation with Mach number of the aerodynamic characteristics of a 10-percent-thick NACA 64A-series airfoil section /

    The effects of amount and type of camber on the variation with Mach number of the aerodynamic characteristics of a 10-percent-thick NACA 64A-series airfoil section / by Summers, James L.

    Published 1950
    Government Document Book
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  2. 2
    Low-speed characteristics of four cambered, 10-percent-thick NACA airfoil sections /

    Low-speed characteristics of four cambered, 10-percent-thick NACA airfoil sections / by McCullough, George B.

    Published 1950
    Government Document Book
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  3. 3
    Investigation of a related series of turbine-blade profiles in cascade /

    Investigation of a related series of turbine-blade profiles in cascade / by Dunavant, James C.

    Published 1956
    Government Document Book
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  4. 4
    Effects of independent variations of Mach number and Reynolds number on the maximum lift coefficients of four NACA 6-series airfoil sections /

    Effects of independent variations of Mach number and Reynolds number on the maximum lift coefficients of four NACA 6-series airfoil sections / by Racisz, Stanley F.

    Published 1952
    Government Document Book
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  5. 5
    The effects of camber on the variation with Mach number of the aerodynamic characteristics of a 10-percent-thick modified NACA four-digit-series airfoil section /

    The effects of camber on the variation with Mach number of the aerodynamic characteristics of a 10-percent-thick modified NACA four-digit-series airfoil section / by Hemenover, Albert D.

    Published 1953
    Government Document Book
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  6. 6
    Effect of blade-thickness taper on axial-velocity distribution at the leading edge of an entrance rotor-blade row with axial inlet, and the influence of this distribution on alignment of the rotor blade for zero angle of attack /

    Effect of blade-thickness taper on axial-velocity distribution at the leading edge of an entrance rotor-blade row with axial inlet, and the influence of this distribution on alignm... by Stanitz, John D.

    Published 1953
    Government Document Book
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  7. 7
    Wind-tunnel investigation of the effect of clipping the tips of triangular wings of different thickness, camber, and aspect ratio - transonic bump method /

    Wind-tunnel investigation of the effect of clipping the tips of triangular wings of different thickness, camber, and aspect ratio - transonic bump method / by Emerson, Horace F.

    Published 1956
    Government Document Book
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  8. 8
    The effect of camber and twist on wing pressure distributions for Mach numbers from 2 to 7.6 /

    The effect of camber and twist on wing pressure distributions for Mach numbers from 2 to 7.6 / by Durgin, Frank H. (Frank Herman)

    Published 1962
    Government Document Book
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  9. 9
    Effect of thickness, camber, and thickness distribution on airfoil characteristics at Mach numbers up to 1.0 /

    Effect of thickness, camber, and thickness distribution on airfoil characteristics at Mach numbers up to 1.0 / by Daley, Bernard N.

    Published 1956
    Government Document Book
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  10. 10
    The effects of body camber on body pressure distributions and wing forces for Mach numbers from 2.0 to 7.6 : Part 1: Experimental data /

    The effects of body camber on body pressure distributions and wing forces for Mach numbers from 2.0 to 7.6 : Part 1: Experimental data / by Durgin, Frank H. (Frank Herman)

    Published 1961
    Government Document Book
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  11. 11
    Effect of linear spanwise variations of twist and circular-arc camber on low-speed static stability, rolling, and yawing characteristics of a 45 degree sweptback wing of aspect ratio 4 and taper ratio 0.6 /

    Effect of linear spanwise variations of twist and circular-arc camber on low-speed static stability, rolling, and yawing characteristics of a 45 degree sweptback wing of aspect rat... by Jaquet, Byron M.

    Published 1952
    Government Document Book
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  12. 12
    Some considerations on two-dimensional thin airfoils deforming in supersonic flow /

    Some considerations on two-dimensional thin airfoils deforming in supersonic flow / by Migotsky, Eugene

    Published 1955
    Government Document Book
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  13. 13
    Contribution to the systematic investigation on Joukowsky profiles /

    Contribution to the systematic investigation on Joukowsky profiles / by Loew, Gottfried

    Published 1928
    Government Document Book
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  14. 14
    Development of a non-autorotative airplane capable of steep landing /

    Development of a non-autorotative airplane capable of steep landing / by Schmidt, Wilhelm

    Published 1931
    Government Document Book
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  15. 15
    Vibration of a wing of finite span in a supersonic flow /

    Vibration of a wing of finite span in a supersonic flow / by Haskind, M. D.

    Published 1950
    Government Document Book
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  16. 16
    Airfoil measurements in the DVL high-speed wind tunnel (2.7-meter diameter) /

    Airfoil measurements in the DVL high-speed wind tunnel (2.7-meter diameter) / by Göthert, B.

    Published 1949
    Government Document Book
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  17. 17
    The transonic characteristics of 38 cambered rectangular wings as varying aspect ratio and thickness as determined by the transonic-bump technique /

    The transonic characteristics of 38 cambered rectangular wings as varying aspect ratio and thickness as determined by the transonic-bump technique / by Nelson, Warren H.

    Published 1955
    Government Document Book
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  18. 18
    General solutions for flow past slender cambered wings with swept trailing edges and calculation of additional loading due to control surfaces /

    General solutions for flow past slender cambered wings with swept trailing edges and calculation of additional loading due to control surfaces / by Klunker, E. B.

    Published 1958
    Government Document Book
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  19. 19
    Effect of reflex camber on the aerodynamic characteristics of a highly tapered moderately swept-back wing at Reynolds numbers up to 8,000,000 /

    Effect of reflex camber on the aerodynamic characteristics of a highly tapered moderately swept-back wing at Reynolds numbers up to 8,000,000 / by Conner, D. William

    Published 1947
    Government Document Book
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  20. 20
    Moments of cambered round bodies /

    Moments of cambered round bodies / by Kempf, Gunther

    Published 1949
    Government Document Book
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