An investigation was conducted to determine the aerodynamic characteristics of a tandem wing configuration. The configuration had a low forward mounted sweptback wing and a high rear mounted sweptforward wing jointed at the wing tip by an end plate. The investigation was conducted at a Mach number of 0.30 at angles of attack up to 20 deg. A comparison of the experimentally determined drag due to lift characteristics with theoretical estimates is also included.


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    Title :

    Aerodynamic characteristics of a tandem wing configuration of a Mach number of 0.30


    Contributors:

    Publication date :

    1975-10-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :