Results of investigation of full scale, nose slot cowlings conducted in NACA 20-ft wind tunnel to furnish information on pressure drop available for cooling; engine conductances from 0 to 0.12 and exit slot conductances from 0 to 0.30 covered.


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    Title :

    Effect of exit-slot position and opening on available cooling pressure for N.A.C.A. Nose-slot cowlings


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:
    Stickle, G.W. (author) / Naiman, I. (author) / Crigler, J.L. (author)


    Publication date :

    1940


    Size :

    12 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English





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