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  1. 61
    Full-scale wind-tunnel and flight tests of a Fairchild 22 airplane equipped with a Fowler flap /
    by Dearborn, C. H
    Published 1936

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  2. 62
    Notes on the calculation of the minimum horizontal tail surface for airplanes equipped with wing flaps /

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  3. 63
    Influence of wing and fuselage on the vertical-tail contribution to the low-speed rolling derivatives of midwing airplane models with 45 degree sweptback surfaces /
    by Wolhart, Walter D
    Published 1951

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  4. 64
    Theoretical aerodynamic characteristics of a family of slender wing-tail-body combinations /
    by Lomax, Harvard
    Published 1951

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  5. 65
    Tail-design requirements for satisfactory spin recovery for personal-owner-type light airplanes /
    by Neihouse, A. I
    Published 1947

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  6. 66
    Wind-tunnel investigation of unshielded horn balances on a horizontal tail surface /
    by Lowry, John G
    Published 1947

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  7. 67
    Effect of horizontal-tail position on the hinge moments of an unbalanced rudder in attitudes simulating spin conditions /

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  8. 68
    Wind-tunnel investigation of effects of unsymmetrical horizontal-tail arrangements on power-on static longitudinal stability of a single-engine airplane model /
    by Purser, Paul E
    Published 1947

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  9. 69
    Measurements of the pressure distribution on the horizontal-tail surface of a typical propeller-driven pursuit airplane in flight
    by Sadoff, Melvin
    Published 1948

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  10. 70
    Effect of tail surfaces on the base drag of a body of revolution at Mach numbers of 1.5 and 2.0 /
    by Spahr, J. Richard
    Published 1951

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