An integrated system for the analysis of supersonic configurations consists of an executive driver and eight basic computer programs that build up force coefficients of an selected configuration. System employs modified linearized theory for calculation of surface pressures and employs supersonic-area-rule concepts in combination with linearized theory for calculation of aerodynamic force coefficients.


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    Titel :

    Aerodynamics of Supersonic Aircraft


    Beteiligte:
    Middleton, W. D. (Autor:in) / Lundry, J. L. (Autor:in) / Coleman, R. G. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.11.1982



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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