Values of derivatives, calculated using linearized theory for compressible flow, presented in form of design charts showing variations of derivatives with Mach number and aspect ratio for nine plan forms. (30¢)


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    Title :

    Summary of lateral-stability derivatives calculated for wing plan forms in supersonic flow


    Additional title:

    NACA -- Report


    Contributors:
    Jones, A.L. (author) / Alksne, A.A. (author)


    Publication date :

    1951


    Size :

    35 pages


    Remarks:

    Charts, Tables, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :