Measurements for range of Mach number up to 0.78; results showed that large increase in drag coefficient beyond critical Mach number indicated by wind tunnel tests was also obtained under flight conditions and that wake width was extended sharply when shock was encountered.


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    Titel :

    Wake measurements behind wing section of fighter airplane in fast dives


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Beeler, D.E. (Autor:in) / Gerard, G. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    8 pages


    Anmerkungen:

    10 Supp plates


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Flight investigation of wing-gun fairings on fighter type airplane

    Nissen, J.M. / White, M.D. | Engineering Index Backfile | 1941