Analysis of flight data to determine wing fuselage aerodynamics center position, zero lift pitching moment coefficients, aircraft pitching moment of inertia, and radius of gyration; pitching moment of inertia determined from flight data for rigid wing conditions agreed with calculations based on ground tests.


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    Title :

    Analysis of horizontal-tail loads in pitching maneuvers on flexible swept-wing jet bomber


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1957


    Size :

    58 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :