Wind tunnel tests were conducted in the Langley 7 x 10 foot wind tunnel at Mach numbers less than 0.20 and at Reynolds numbers less than 3.74 million. The effect of the aft area on the 45 deg swept wing longitudinal aerodynamic characteristics at low subsonic speeds and at an angle of attack range from approximately -2 deg to 28 deg was studied. The data are presented without analysis.


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    Title :

    Longitudinal aerodynamic characteristics of 45 deg swept wings at Mach approximately 0


    Contributors:

    Publication date :

    1976-09-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :


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