Solution by iteration estimates performance of twisted and cambered wings of arbitrary planform. SUBAER based on linearized theory lifting-surface solution provides spanwise distribution of theoretical leading edge thrust, in addition to surface distribution of perturbation velocities. Program written in FORTRAN IV.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Wing Subsonic Aerodynamic Performance Estimates


    Beteiligte:
    Carlson, H. W. (Autor:in) / Walkley, K. B. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1983-08-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Aerodynamic Optimization for Subsonic Fixed Wing UAV

    Masood, Khayyam / Wei, Zhang | AIAA | 2013


    Aerodynamic Optimization of Subsonic Flying Wing Configurations

    Mialon, B. / Fol, T. / Bonnaud, C. et al. | British Library Conference Proceedings | 2002


    Aerodynamic Optimization of Subsonic Flying Wing Configurations

    Mialon, Bruno / Fol, Thierry / Bonnaud, Cyril | AIAA | 2002


    Unsteady aerodynamic loading computation for subsonic oscillating wing

    Li, H. / Zhpu, W. | British Library Online Contents | 1995


    Aerodynamic design challenges of the Blended-Wing-Body subsonic transport

    Roman, D. / Allen, J. / Liebeck, R. | AIAA | 2000