Effect of inlet velocity ratio, angle of attack, radiator resistance, and propeller operation on pressure recovery at radiator, on drag of cooling installation, and on critical speed of ducts. (Advance Restricted Report L4H15 Oct 1944)


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    Title :

    Full-scale wind-tunnel investigation of forward underslung cooling-air ducts


    Additional title:

    Nat Advisory Committee Aeronautics -- Wartime Report


    Contributors:


    Publication date :

    1944


    Size :

    19 pages


    Remarks:

    33 supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English





    Wind-tunnel investigation of rear underslung fuselage ducts

    Czarnecki, K.R. / Nelson, W.J. | Engineering Index Backfile | 1943



    Wind-Tunnel Investigation of Rear Underslung Fuselage Ducts

    K. R. Czarnecki / W. J. Nelson | NTIS | 1943


    Wind-tunnel investigation of rear underslung fuselage ducts

    Czarnecki, K. R. / Nelson, W. J. | TIBKAT | 1943