Lateral-directional handling qualities for Class 4 airplanes in Flight Phase Category A were investigated in the USAF/CAL variable stability NT-33A airplane. The primary purpose was to extend the data base for roll-sideslip coupling requirements specified by MIL-F-8785B(ASG) for this Class of airplanes. Other purposes included evaluation of the minimum Dutch roll frequency and damping requirements of MIl-F-8785B (ASG) for Class 4 airplanes in Flight Phase Category A and an investigation of the applicability of MIL-F-83300 roll-sideslip requirements to airplanes in high speed flight conditions. (Author)


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    Titel :

    Evaluation of Lateral-Directional Handling Qualities and Roll-Sideslip Coupling of Fighter Class Airplanes


    Beteiligte:
    E. M. Boothe (Autor:in) / M. L. Parrag (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    150 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    BULL, GIFFORD | SAE Technical Papers | 1960


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    Bull, G. | Engineering Index Backfile | 1960