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)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

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


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Wartime Report


    Beteiligte:
    Nelson, W.J. (Autor:in) / Czarnecki, K.R. (Autor:in) / Harrington, R.D. (Autor:in)


    Erscheinungsdatum :

    1944


    Format / Umfang :

    19 pages


    Anmerkungen:

    33 supp plates


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    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