Report presents the results of a comprehensive experimental study carried out at full scale in the NACA 20-foot wind tunnel, the general purpose of which is to furnish information in regard to the functioning of the power plant and propeller unit under different conditions. This report deals particularly with the problem of the cooling of an airplane engines on the ground. The influence of different nose forms, skirts, flaps, propellers, spinners, and special blowers has been investigated.


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    Title :

    Cooling of Airplane Engines at Low Air Speeds


    Contributors:

    Publication date :

    1937-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English



    Cooling of airplane engines at low air speeds

    Theodorsen, T. / Brevoort, M.J. / Stickle, G.W. | Engineering Index Backfile | 1937


    Cooling of airplane engines at low air speeds

    Theodorsen, T. / Brevoort, M.J. / Stickle, G. | Engineering Index Backfile | 1937


    Cooling of airplane engines at low air speeds

    Theodorsen, T. / Brevoort, M.J. / Stickle, G.W. | Engineering Index Backfile | 1937


    Airplane engines

    Engineering Index Backfile | 1932


    Airplane engines

    Engineering Index Backfile | 1932