The locally linearized longitudinal and lateral-directional aerodynamic stability and control derivatives for the X-29A aircraft were calculated for altitudes ranging from sea level to 50,000 ft, Mach numbers from 0.2 to 1.5, and angles of attack from -5 deg to 25 deg. Several other parameters were also calculated, including aerodynamic force and moment coefficients, control face position, normal acceleration, static margin, and reference angle of attack.


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    Titel :

    Locally Linearized Longitudinal and Lateral-Directional Aerodynamic Stability and Control Derivaties for the X-29A Aircraft


    Beteiligte:
    G. D. Budd (Autor:in)

    Erscheinungsdatum :

    1984


    Format / Umfang :

    480 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch