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  1. 41
    Development of the rules governing the strength of airplanes /
    by Küssner, H. G
    Published 1933

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  2. 42
    Pressure distribution on wings in reversed flow /
    by Naumann, A
    Published 1942

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  3. 43
    The effect of camber and twist on wing pressure distributions for Mach numbers from 2 to 7.6
    Published 1962

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  4. 44
    External loads and aircraft strength,
    by Gudkov, Aleksandr Ivanovich
    Published 1973

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  5. 45
    Extreme value analysis and its application to c.g. vertical accelerations measured on transport airplanes of type C-130 /
    by Buxbaum, O
    Published 1971

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  6. 46
    Horizontal tail loads in maneuvering flight /

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  7. 47
    First-order theory for unsteady motion of thin wings at supersonic speeds /
    by Moskowitz, Barry
    Published 1950

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  8. 48
    Theoretical lift and damping in roll of thin sweptback tapered wings with raked-in and cross-stream wing tips at supersonic speeds /
    by Margolis, Kenneth
    Published 1950

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  9. 49
    Pressure distribution and damping in steady roll at supersonic Mach numbers of flat swept-back wings with subsonic edges /
    by Walker, Harold J
    Published 1950

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  10. 50
    Comparison between theory and experiment for wings at supersonic speeds /
    by Vicenti, Walter G
    Published 1950

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