Power-off tests conducted to determine dynamic stability of model with 42° swept back wing of aspect ratio 5.9 and taper ratio 0.45; results showed that, although wing alone was statically unstable longitudinally at moderate and high lift coefficients, complete model was practically stable over lift range for some horizontal tail positions.


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    Titel :

    Flight tests of airplane model with 42° swept-back wing in Langley free-plight tunnel


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Maggin, B. (Autor:in) / Bennett, C.V. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    14 pages


    Anmerkungen:

    14 Supp plates


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :