Aerodynamic derivatives were obtained for the M2-F2 lifting body flight vehicle in the subsonic flight region between Mach numbers of 0.41 and 0.64 and altitudes of 7000 feet to 45,000 feet. The derivatives were determined by a flight time history curve-fitting process utilizing a hybrid computer. The flight-determined derivatives are compared with wind-tunnel and predicted values. Modal-response characteristics, calculated from the flight derivatives, are presented.


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    Title :

    Flight-determined aerodynamic stability and control derivatives of the M2-F2 lifting body vehicle at subsonic speeds


    Contributors:

    Publication date :

    1971-12-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :