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  1. 1
    The effects of sideslip, aspect ratio, and mach number on the lift and pitching moment of triangular, trapezoidal, and related plan forms in supersonic flow /

    The effects of sideslip, aspect ratio, and mach number on the lift and pitching moment of triangular, trapezoidal, and related plan forms in supersonic flow / by Jones, A. L. (Arthur Leslie)

    Published 1949
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  2. 2
    Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1,800,000 to 11,000,000 /

    Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1,800,000 to 11,000,000 / by Schaefer, Raymond F.

    Published 1949
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  3. 3
    Some effects of varying the damping in pitch and roll on the flying qualities of a small single-rotor helicopter /

    Some effects of varying the damping in pitch and roll on the flying qualities of a small single-rotor helicopter / by Reeder, John P.

    Published 1952
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  4. 4
    Pitching-moment derivatives Cmq and Cma at supersonic speeds for a slender-delta-wing and slender-body combination and approximate solutions for broad-delta-wing and slender-body combinations /

    Pitching-moment derivatives Cmq and Cma at supersonic speeds for a slender-delta-wing and slender-body combination and approximate solutions for broad-delta-wing and slender-body c... by Henderson, Arthur

    Published 1951
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  5. 5
    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
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  6. 6
    Effects of compressibility on the performance of two full-scale helicopter rotors /

    Effects of compressibility on the performance of two full-scale helicopter rotors / by Carpenter, Paul J.

    Published 1951
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  7. 7
    Lift and pitching derivatives of thin sweptback tapered wings with streamwise tips and subsonic leading edges at supersonic speeds /

    Lift and pitching derivatives of thin sweptback tapered wings with streamwise tips and subsonic leading edges at supersonic speeds / by Malvestuto, Frank S.

    Published 1951
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  8. 8
    Wind-tunnel investigation at low speed of a 45 degree sweptback untapered semispan wing of apsect ratio 1.59 equipped with various 25-percent-chord plain flaps /

    Wind-tunnel investigation at low speed of a 45 degree sweptback untapered semispan wing of apsect ratio 1.59 equipped with various 25-percent-chord plain flaps / by Johnson, Harold S.

    Published 1950
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  9. 9
    Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7 /

    Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7 / by Turner, M. J.

    Published 1950
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  10. 10
    Single-degree-of-freedom-flutter calculations for a wing in subsonic potential flow and comparison with an experiment /

    Single-degree-of-freedom-flutter calculations for a wing in subsonic potential flow and comparison with an experiment / by Runyan, Harry L.

    Published 1951
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  11. 11
    An investigation of the effects of jet-outlet cut-off angle on thrust direction and body pitching moment /

    An investigation of the effects of jet-outlet cut-off angle on thrust direction and body pitching moment / by Blackaby, James R.

    Published 1951
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  12. 12
    Three-dimensional unsteady lift problems in high-speed flight : the triangular wing /

    Three-dimensional unsteady lift problems in high-speed flight : the triangular wing / by Lomax, Harvard

    Published 1951
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  13. 13
    Effect of horizontal-tail location on low-speed static longitudinal stability and damping in pitch of a model having 45° sweptback wing and tail surfaces /

    Effect of horizontal-tail location on low-speed static longitudinal stability and damping in pitch of a model having 45° sweptback wing and tail surfaces / by Lichtenstein, Jacob H.

    Published 1951
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  14. 14
    The indicial lift and pitching moment for a sinking or pitching two-dimensional wing flying at subsonic or supersonic speeds /

    The indicial lift and pitching moment for a sinking or pitching two-dimensional wing flying at subsonic or supersonic speeds / by Lomax, Harvard

    Published 1951
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  15. 15
    The effect of a simulated propeller slipstream on the aerodynamic characteristics of an unswept wing panel with and without nacelles at Mach numbers from 0.30 and 0.86 /

    The effect of a simulated propeller slipstream on the aerodynamic characteristics of an unswept wing panel with and without nacelles at Mach numbers from 0.30 and 0.86 / by Jordan, Gareth H.

    Published 1952
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  16. 16
    Theoretical investigation of longitudinal response characteristics of a swept-wing fighter airplane having a normal-acceleration control system and a comparison with other types of systems /

    Theoretical investigation of longitudinal response characteristics of a swept-wing fighter airplane having a normal-acceleration control system and a comparison with other types of... by Stokes, Fred H.

    Published 1954
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  17. 17
    Lift and pitching moment at supersonic speeds due to constant vertical acceleration for thin sweptback tapered wings with streamwise tips. : Supersonic leading and trailing edges /

    Lift and pitching moment at supersonic speeds due to constant vertical acceleration for thin sweptback tapered wings with streamwise tips. : Supersonic leading and trailing edges / by Cole, Isabella J.

    Published 1954
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  18. 18
    Effect of a rapid blade-pitch increase on the thrust and induced-velocity response of a full-scale helicopter rotor /

    Effect of a rapid blade-pitch increase on the thrust and induced-velocity response of a full-scale helicopter rotor / by Carpenter, Paul J.

    Published 1953
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  19. 19
    A theoretical investigation of the aerodynamics of wing-tail combinations performing time-dependent motions at supersonic speeds /

    A theoretical investigation of the aerodynamics of wing-tail combinations performing time-dependent motions at supersonic speeds / by Martin, John C.

    Published 1954
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  20. 20
    A flight investigation of the effect of steady rolling on the natural frequencies of a body-tail combination /

    A flight investigation of the effect of steady rolling on the natural frequencies of a body-tail combination / by Bergrun, Norman R.

    Published 1953
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