The article presents the results of an experimental study of the damping moment coefficients of the configuration of supersonic airliner models with small wing aspect ratios in a supersonic wind tunnel. A comparison of experimental and calculated data is presented.


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    Title :

    A Study of the Damping Characteristics on Models of Supersonic Airlines at Supersonic Speeds


    Contributors:

    Publication date :

    1974


    Size :

    11 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Supersonic airlines

    Online Contents | 1994


    Supersonic airlines

    Online Contents | 1994


    Supersonic airlines

    Online Contents | 1994


    Supersonic airlines

    Online Contents | 1994