Validity and applicability of static margin parameter defining stability of flexible aircraft is shown to be restricted to conventional aircraft; alternative suggestions for definition of static margin are put forward which can be equally applied to conventional flexible aircraft of past and integrated flexible aircraft of future; calculations carried out on simple slender plate models with linear and nonlinear aerodynamic forces to assess their static stability characteristics. Pt 1-2 indexed in Engineering Index 1961 p 47.


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    Titel :

    Static aeroelasticity of slender configurations -- 3


    Weitere Titelangaben:

    Aeronautical Quarterly


    Beteiligte:
    Hancock, G.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1963


    Format / Umfang :

    30 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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    Static Aeroelasticity Computations for Flexible Wing-Body-Control Configurations

    Byun, C. / Guruswamy, G. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 1996



    Static aeroelastic deformation of slender configurations

    Hancock, G.J. | Engineering Index Backfile | 1961