This report is on the changes in forces on each wing of a biplane cellule when either the stagger or the gap is varied. Since each test was carried up to a 90 degree angle of attack, the results may be used in the study of stalled flight and of spinning as well as in the structural design of biplane wings.


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    Title :

    Wind Tunnel Pressure Distribution Tests on a Series of Biplane Wing Models


    Contributors:

    Publication date :

    1929-07-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English