New method of calculation makes direct use of actual airplane polars without approximations; procedure based on extension of Eiffel-Rith coordinate system, and all scales can be incorporated in simple transparent chart, thereby eliminating necessity for special prepared graph paper; compressibility effects are taken into account through use of constant altitude variable Mach number polars which are derived from constant Mach number polars of true airplane. (see also J Aeronautical Sciences v 11 n 4 Oct 1944 p 329-38)


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    Title :

    Logarithmic performance computation


    Additional title:

    Aircraft Eng


    Contributors:
    Foa, J.V. (author) / Leadon, B.M. (author)

    Published in:

    Publication date :

    1944


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Logarithmic performance computation

    Foa, J.V. / Leadon, B.M. | Engineering Index Backfile | 1944





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