The wing differential pressure distributions of two vehicles are predicted using FLEXSTAB. Three space shuttle configurations were investigated. Comparisons were made of wind tunnel and analytical data for a selected range of angle of attack, angle of sideslip, and Mach number. A drone-type vehicle was investigated and comparisons were made between flight and analytical data of wing pressure distributions and static longitudinal stability derivatives.


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    Titel :

    FLEXSTAB analysis


    Beteiligte:

    Erscheinungsdatum :

    1976-02-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    FLEXSTAB Analysis

    H. E. Lowder | NTIS | 1976


    Estimate of Orbiter static aeroelasticity properties via FLEXSTAB

    Cavin, R. K., III / Holyoak, J. N. | NTRS | 1978




    ANALYSIS DEVICE, ANALYSIS METHOD, AND ANALYSIS PROGRAM

    AOKI YUKARI / SAKAKIBARA HAJIME / CHIGA MAKOTO | Europäisches Patentamt | 2016

    Freier Zugriff