Investigation on bomber aircraft to determine overall magnitude of aeroelastic effects on bending and shear strains in rough air show that amplification of strain per unit acceleration in gusts increases with outboard spanwise station to maximum amplification factor of 2.72.


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    Title :

    Effects of airplane flexibility on wing strains in rough air at 5,000 feet as determined by flight tests of large swept-wing airplane


    Additional title:

    NACA -- Tech Note


    Contributors:
    Rhyne, R.H. (author) / Murrow, H.N. (author)

    Published in:

    Publication date :

    1957


    Size :

    32 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :