Performances obtainable at different altitudes with various assumed ratios of actual engine power at altitude to total weight of airplane, are computed for DeHaviland-Four, which is taken as typical of present practice.


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    Title :

    Maintaining airplane engine power at great altitudes


    Additional title:

    Jl. Soc. Automotive Engrs


    Contributors:
    Clark, V.E. (author)


    Publication date :

    1920


    Size :

    5 pages


    Remarks:

    7 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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