Calculation of lift and pitching moments due to angle of attack and steady pitching velocity at supersonic speeds for thin sweptback tapered wings with streamwise tips and supersonic leading and trailing edges.


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    Title :

    Calculation of lift and pitching moments due to angle of attack and steady pitching velocity at supersonic speeds for thin sweptback tapered wings with streamwise tips and supersonic leading and trailing edges


    Additional title:

    NACA -- Tech Note


    Contributors:
    Martin, J.C. (author) / Margolis, K. (author) / Jeffreys, I. (author)


    Publication date :

    1952


    Size :

    116 pages


    Remarks:

    Diagrams, Charts, Tables


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :