Longitudinal and lateral stability and control characteristics of swept wing fighter aircraft


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    Title :

    A summary of the longitudinal and lateral stability and control characteristics obtained from rocket-model tests of a swept-wing fighter-type airplane at Mach numbers from 0.5 to 1.9


    Contributors:

    Publication date :

    1957-02-27


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English