The application of the FLEXSTAB system to analyze airplane configurations is explained with examples of demonstration cases: Dart Model I, Dart Model II, the Boeing 707-320B, the Boeing 2707-300PT(SST), and the Lockheed YF-12A. The Dart Models I and II are two very simple configurations used to illustrate the program input and usage. The modeling and the preparation of input data for the 707, SST and YF-12A configurations is discussed, and the selected results are presented in a tabular form. A comparison of results with other sources is included for the 707 and SST models. In addition, a comparison of the FLEXSTAB results for pressure and force distribution with the experimental results for an arrow-wing configuration (obtained under NASA Contract NASI-12875) are included.


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    Titel :

    A Method for Predicting the Stability Characteristics of an Elastic Airplane. Volume IV. FLEXSTAB 1.02.00 Demonstration Cases and Results


    Beteiligte:
    G. M. Dornfeld (Autor:in) / K. G. Bhatia (Autor:in) / R. E. Maier (Autor:in) / R. N. Snow (Autor:in) / D. A. Van Rossum (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    329 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch