Development of formulas for determination of major airplane performance characteristics making no assumption regarding altitude of airplane at which maximum rate of climb occurs, but finding altitude at which excess thrust horsepower is maximum; performance in terms of parasite loading, effective span loading and thrust horsepower loading.


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    Title :

    General formulas and charts for calculation of airplane performance


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1932


    Size :

    50 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English






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