It is assumed that aircraft dives at constant angle, propeller exerting constant thrust; at beginning of dive aircraft has zero vertical velocity; throughout dive, weight and resistance coefficient of aircraft are constant. English abstract from Luftwissen v 10 n 2 Feb 1943 p 51-2. (Abstract Sec) (See also Engrs' Digest v 4 n 9 Sept 1943 p 271-3)


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    Title :

    Diving speed calculation


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:

    Published in:

    Publication date :

    1943


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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