Digital Datcom is evaluated as a tool for predicting the subsonic aerodynamic characteristics of forward-swept-wing aircraft. Comparisons are made with wing-alone and wing-body wind tunnel data as well as three complete configurations: two generic (one being sweptback) and the X-29. Good agreement between tested and predicted longitudinal and lateral-directional stability derivatives is noted but the zero-lift pitching, moment is not well estimated for X-29. Control derivative estimates match test data well except for aileron-induced yawing moment.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    A subsonic analysis of digital datcom using several forward swept wing configurations


    Weitere Titelangaben:

    Eine subsonische Analyse von digitalem Datcom mittels mehrerer Konfigurationen von sich nach vorne bewegenden Fluegeln


    Beteiligte:
    Blake, W.B. (Autor:in) / Sharpes, D.G. (Autor:in)


    Erscheinungsdatum :

    1987


    Format / Umfang :

    8 Seiten, 20 Bilder, 1 Tabelle, 8 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Computational Analysis of Subsonic Vortex Interaction on Multi Swept Delta Wing Configurations

    Visonneau, Michel / Guilmineau, Emmanuel / Wackers, Jeroen | AIAA | 2022


    Vortical Flowfield Structure at Forward Swept-Wing Configurations

    Christian Breitsamter / Boris Laschka | AIAA | 2001



    Aerodynamic Characteristics of Canard-Forward Swept Wing Aircraft Configurations

    Zhang, G. Q. / Yu, S. C. M. / Chien, A. et al. | AIAA | 2013


    Forward swept wing design

    KRONE, JR., N. | AIAA | 1980