Results of tests completed at University of Detroit 7 by 10-ft wind tunnel to determine effects of double split flap dive brakes on lift, drag, and pitching moment characteristics of airfoil and airplane model. Before Inst Aeronautical Sciences.


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    Title :

    Effect of dive brakes on airfoil and airplane characteristics


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1944


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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