Longitudinal and lateral stability and control derivatives for X-15A aircraft at supersonic and hypersonic speeds - comparison of theoretical results with wind tunnel testing


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    Title :

    Theoretical Stability Derivatives for the X-15 Research Airplane at Supersonic and Hypersonic Speeds Including a Comparison with Wind-tunnel Results


    Contributors:

    Publication date :

    1960-08-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English