Application of theory of dynamic longitudinal stability, based on assumption of small oscillations, to oscillations airplane is likely to undergo in flight; period and damping determined by direct measurements of oscillations in flight.


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    Title :

    Comparison between theoretical and measured longitudinal stability characteristics of airplane


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1932


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




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    Metcalf, A.G.B. | Engineering Index Backfile | 1937


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