Newtonian flow theory for conical flow field is applied to estimate thickness effect on force of slender delta wings at moderate angle of attack; assuming shock shape in cross plane perpendicular to wings, pressure coefficient for wings with either diamond or lens-type cross section is obtained; comparison with other theoretical and experimental work is made; it is concluded that thickness of wing diminishes normal force for smaller values of parameter Omega but increases it for larger values where Omega is similarity parameter introduced by A.F.Messiter.


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    Titel :

    Thickness effect on force of slender delta wings in hypersonic flow


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Hida, K. (Autor:in)

    Erschienen in:

    AIAA Journal ; 3 , n 3


    Erscheinungsdatum :

    1965


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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