Flight test program highlights are discussed for the X-29 high angle-of-attack (AOA) aircraft. The AOA envelope extended from 10 to 66 deg; the X-29 exhibited precise pitch control, allowing AOA to be maintained within 1 deg during stabilized points as well as permitting rapid recoveries from all AOAs. Attention is given to controllability degradation above 40-deg AOA due to asymmetric yawing moments. The use of this aircraft as a fundamental research tool which complements analytical methods is powerfully justified by the obviation of scaling effects.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    X-29 high angle of attack


    Beteiligte:

    Kongress:

    Symposium of the 1990 report to the Aerospace Profession; Society of Experimental Test Pilots


    Erscheinungsdatum :

    1990-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    High Angle of Attack Aerodynamics

    Champigny, P. / AGARD; Fluid Dynamics Panel | British Library Conference Proceedings | 1994


    High Angle of Attack - Aerodynamics

    John E. Lamar | NTRS | 1992



    High Angle of Attack Aerodynamics

    P. Champigny | NTIS | 1994


    ATTACK ANGLE ESTIMATION METHOD AND ATTACK ANGLE ESTIMATION DEVICE

    KUNIYUKI SHOYA / HONDO TAKATOSHI / SUZUKI MITSUGI et al. | Europäisches Patentamt | 2023

    Freier Zugriff