Closed-form formulas for the effects of finite afterbodies on the longitudinal center of pressure location in the presence of a wing at supersonic speeds are presented, along with solutions for the case of negative afterbodies. A double integral is developed for the case of subsonic and supersonic leading edges and no afterbody and full afterbody. Attention is also given to the full/infinite body case, noting that a proportional variation of the pitching moment with the lift is found.


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    Titel :

    Supersonic wing-body center of pressure with finite afterbodies


    Beteiligte:
    Vira, N. R. (Autor:in) / Fan, D.-N. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.08.1982


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



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