General equations for reduction of flight test climb data to standard air conditions are given, indicating how airplane and engine characteristics affect necessary rate of climb corrections; charts are given to provide aid in reduction of climb data of airplanes having modern engine installations.


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    Title :

    Reduction of flight test climb data to standard air conditions


    Additional title:

    J Aeronautical Sciences


    Contributors:
    White, R.J. (author)

    Published in:

    Publication date :

    1939


    Size :

    6 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :