Pointed wing of aspect ratio 4 was modified by clipping small portions off wing tips to form wings with aspect ratios of 3.50, 3.25, and 3.00; first one was extensively tested as complete model with various horizontal-and vertical-tail combinations.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Static longitudinal characteristics at high subsonic speeds of complete airplane model with highly tapered wing having 0.80 chord line unswept and with several tail configurations


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Goodson, K.W. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    57 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :