Wind tunnel tests to improve static directional stability of unswept-wing aircraft at mach 0.8-2.2


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    WIND-TUNNEL INVESTIGATION OF DEVICES TO IMPROVE STATIC DIRECTIONAL STABILITY OF AN UNSWEPT-WING AIRPLANE MODEL AT MACH NUMBERS FROM 0.8 TO 2.2


    Contributors:

    Publication date :

    1958-12-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English