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  1. 21
    Effect of fabric deflection at high speeds on the aerodynamic characteristics of the horizontal tail surface of an SB2D-1 airplane /

    Effect of fabric deflection at high speeds on the aerodynamic characteristics of the horizontal tail surface of an SB2D-1 airplane / by Schueller, Carl F.

    Published 1945
    Government Document Book
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  2. 22
    Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil /

    Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil / by Bird, J. D.

    Published 1945
    Government Document Book
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  3. 23
    Hinge moments of sealed-internal-balance arrangements for control surfaces. : 1 - Theoretical investigation /

    Hinge moments of sealed-internal-balance arrangements for control surfaces. : 1 - Theoretical investigation / by Murray, Harry E.

    Published 1945
    Government Document Book
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  4. 24
    Effect of hinge-moment parameters on elevator stick forces in rapid maneuvers /

    Effect of hinge-moment parameters on elevator stick forces in rapid maneuvers / by Jones, Robert T. (Robert Thomas), 1910-1999

    Published 1944
    Government Document Book
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  5. 25
    Wind-tunnel investigation of control-surface characteristics. : 20 - Plain and balanced flaps on an NACA 0009 rectangular semispan tail surface /

    Wind-tunnel investigation of control-surface characteristics. : 20 - Plain and balanced flaps on an NACA 0009 rectangular semispan tail surface / by Garner, I. Elizabeth

    Published 1944
    Government Document Book
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  6. 26
    Effect of elevator-profile modifications and trailing-edge strips on elevator hinge-moment and other aerodynamic characteristics of a full-scale horizontal tail surface /

    Effect of elevator-profile modifications and trailing-edge strips on elevator hinge-moment and other aerodynamic characteristics of a full-scale horizontal tail surface / by Schueller, Carl F.

    Published 1945
    Government Document Book
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  7. 27
    Calculation of stick forces for an elevator with a spring tab /

    Calculation of stick forces for an elevator with a spring tab / by Greenberg, Harry

    Published 1944
    Government Document Book
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  8. 28
    Wind-tunnel investigation of control-surface characteristics. : 14 - NACA 0009 airfoil with a 20-percent-chord double plain flap /

    Wind-tunnel investigation of control-surface characteristics. : 14 - NACA 0009 airfoil with a 20-percent-chord double plain flap / by Sears, Richard I.

    Published 1943
    Government Document Book
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  9. 29
    Rolling, yawing, and hinge moments produced by rectangular ailerons (correlating Technical Reports nos. 298, 343, and 370) /

    Rolling, yawing, and hinge moments produced by rectangular ailerons (correlating Technical Reports nos. 298, 343, and 370) / by Heald, R. H.

    Published 1933
    Online Access
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  10. 30
    Wind-tunnel investigation of control-surface characteristics. : 19 - A double flap with an overhang and an internal aerodynamic balance /

    Wind-tunnel investigation of control-surface characteristics. : 19 - A double flap with an overhang and an internal aerodynamic balance / by Liddell, Robert B.

    Published 1944
    Government Document Book
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  11. 31
    Limitations of lifing-line theory for estimation of aileron hinge-moment characteristics /

    Limitations of lifing-line theory for estimation of aileron hinge-moment characteristics / by Swanson, Robert S.

    Published 1943
    Government Document Book
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  12. 32
    Wind-tunnel investigation of a tapered wing with a plug-type spoiler-slot aileron and full-span slotted flaps /

    Wind-tunnel investigation of a tapered wing with a plug-type spoiler-slot aileron and full-span slotted flaps / by Lowry, John G.

    Published 1942
    Government Document Book
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  13. 33
    Wind-tunnel investigation of shielded horn balancees and tabs on a 0.7-scale model of XF6F vertical tail surface /

    Wind-tunnel investigation of shielded horn balancees and tabs on a 0.7-scale model of XF6F vertical tail surface / by Lowry, John G.

    Published 1944
    Search for the full-text version of this title in HathiTrust
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  14. 34
    Wind-tunnel investigation of control-surface characteristics. : 26 - Pressure distribution over an NACA 0009 airfoil with 0.30-airfoil-chord beveled-trailing-edge flaps /

    Wind-tunnel investigation of control-surface characteristics. : 26 - Pressure distribution over an NACA 0009 airfoil with 0.30-airfoil-chord beveled-trailing-edge flaps / by Hoggard, H. Page

    Published 1944
    Government Document Book
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  15. 35
    Wind-tunnel investigation of control-surface characteristics. : 5 - The use of a beveled trailing edge to reduce the hinge moment of a control surface /

    Wind-tunnel investigation of control-surface characteristics. : 5 - The use of a beveled trailing edge to reduce the hinge moment of a control surface / by Jones, Robert T. (Robert Thomas), 1910-1999

    Published 1942
    Government Document Book
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  16. 36
    A flight investigation of internally balanced sealed ailerons /

    A flight investigation of internally balanced sealed ailerons / by Williams, W. C.

    Published 1941
    Government Document Book
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  17. 37
    Wind-tunnel tests of a piston-type control booster on an airfoil and aileron model /

    Wind-tunnel tests of a piston-type control booster on an airfoil and aileron model / by Bird, J. D.

    Published 1943
    Government Document Book
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  18. 38
    Wind-tunnel tests of hinge-moment characteristics of spring-tab ailerons /

    Wind-tunnel tests of hinge-moment characteristics of spring-tab ailerons / by Imlay, Frederick H.

    Published 1944
    Government Document Book
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  19. 39
    Wind-tunnel tests of ailerons at various speeds. : 3 - Ailerons of 0.20 airfoil chord and true contour with 0.35-aileron-chord Frise balance on the NACA 23012 airfoil /

    Wind-tunnel tests of ailerons at various speeds. : 3 - Ailerons of 0.20 airfoil chord and true contour with 0.35-aileron-chord Frise balance on the NACA 23012 airfoil / by Letko, W.

    Published 1943
    Government Document Book
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  20. 40
    Wind-tunnel investigation of control-surface characteristics. : 15 - Various contour modifications of a 0.30-airfoil-chord plain flap on an NACA 66(215)-014 airfoil /

    Wind-tunnel investigation of control-surface characteristics. : 15 - Various contour modifications of a 0.30-airfoil-chord plain flap on an NACA 66(215)-014 airfoil / by Weil, Joseph

    Published 1943
    Government Document Book
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