Tests to determine aerodynamic characteristics of semi-span tail surface of fighter type airplane were carried to maximum Mach number of 0.7 except for model configurations for which maximum allowable loads were reached at lower speeds; results show effects of elevator nose shape, elevator trailing edge angle, and trailing edge strips.


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    Titel :

    Tests of full-scale horizontal tail surface in Langley 16-foot high-speed tunnel


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Schueller, C.F. (Autor:in) / Korycinski, P.F. (Autor:in) / Strass, H.K. (Autor:in)


    Erscheinungsdatum :

    1946


    Format / Umfang :

    24 pages


    Anmerkungen:

    Supp sheets, Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch