Equations of motion derived for aircraft of nearly circular cross section, such as missiles; it is shown that considerations of steady roll and lack of circular symmetry of cross section lead to Mathieu equations; application of aerodynamic force derivatives for flight not near flutter speed has resulted in theoretical predictions that agree satisfactorily with flight experience.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    On flight dynamics of slender special-purpose aircraft


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Rosenberg, R.M. (Autor:in) / Stoner, G. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1952


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    On the flight dynamics of slender special-purpose aircraft

    Rosenberg, Reinhardt / Stoner, George | TIBKAT | 1952


    Flight testing H.P.115 slender wing aircraft

    Henderson, J.M. | Engineering Index Backfile | 1963


    Some design aspects of slender aircraft for supersonic flight

    Küchemann, D. / Weber, J. | TIBKAT | 1974


    Rapid prediction of slender-wing aircraft dynamics

    ERICSSON, L. / KING, H. | AIAA | 1990