A performance modeling concept previously applied to an F-104F G and a YF-12C airplane was applied to an F-111A airplane. This application extended the concept to an airplane with variable sweep wings. The performance model adequately matched flight test data for maneuvers flown at different wing sweep angles at maximum afterburning and intermediate power settings. For maneuvers flown at less than intermediate power, including dynamic maneuvers, the performance model was not validated because the method used to correlate model and in-flight power setting was not adequate. Individual dynamic maneuvers were matched sucessfully by using adjustments unique to each maneuver.


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    Titel :

    Application of a Performance Modeling Technique to an Airplane with Variable Sweep Wings


    Beteiligte:
    P. C. Redin (Autor:in)

    Erscheinungsdatum :

    1981


    Format / Umfang :

    33 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Aircraft with Variable-Sweep Wings

    Page, R.K. | Emerald Group Publishing | 1965


    Aircraft with variable-sweep wings

    Page, R.K. | Engineering Index Backfile | 1965


    Application of Variable-Sweep Wings to Commuter Aircraft

    A. W. Robins / F. L. Beissner / W. A. Lovell et al. | NTIS | 1983