The paper discusses longitudinal static stability of simplified aerodynamic configurations in extreme ground effect. Static stability margin, defined as the difference between abscissas of aerodynamic centre of height and that of pitch, is determined as a function of parameters of the lifting system. Aerodynamics of low flying wing elements are described by means of the extreme ground effect theory, whereas characteristics of the highly mounted tail are determined with use of the lifting line approach. Qualitative analysis is carried out of the influence of different parameters upon static stability of wing-in-ground effect aerodynamic configurations. Discussion of the study is preceeded by a survey of relevant references.


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    Titel :

    Stability of a simple lifting configuration in extreme ground effect


    Weitere Titelangaben:

    Stabilität einer einfachen, auftriebserzeugenden Konfiguration in extremem Bodeneffekt


    Beteiligte:


    Erscheinungsdatum :

    1997


    Format / Umfang :

    13 Seiten, 11 Bilder, 32 Quellen



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Stability of a Simple Lifting Configuration in Extreme Ground Effect

    Rozhdestvensky, K. V. / Royal Institution of Naval Architects / Royal Aeronautical Society; Rapid Marine Transport Group et al. | British Library Conference Proceedings | 1997


    Lifting Line in Extreme Ground Effect

    Rozhdestvensky, K. V. / European Association of Aerospace Students | British Library Conference Proceedings | 2002


    A Parametric Analysis of A Flying Wing Configuration in Extreme Ground Effect

    Rozhdestvensky, K. V. / University of New South Wales; Department of Naval Architecture | British Library Conference Proceedings | 1996


    Lifting Surfaces in Ground Effect

    Tuck, E. O. / Standingford, D. W. F. / University of New South Wales; Department of Naval Architecture | British Library Conference Proceedings | 1996


    Ground effect on the lifting rotor

    Zbrozek, J. K. | TIBKAT | 1950