Report describes transonic wind-tunnel tests of oblique, pivotable wing fitted to 0.087-scale model of F-8 airplane. Purpose of tests to study performance and stability characteristics. Conducted to determine whether placement of pivot at higher position above fuselage than previously results in less side force and yawing moment than observed in previous tests at low speeds.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Transonic Wind-Tunnel Test Of An Oblique Wing


    Beteiligte:
    Kennelly, R. A. (Autor:in) / Strong, J. M. (Autor:in) / Carmichael, R. L. (Autor:in) / Kroo, I. M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1992-12-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Transonic Wind Tunnel Test of a 14 Percent Thick Oblique Wing

    R. A. Kennelly / I. M. Kroo / J. M. Strong et al. | NTIS | 1990


    Transonic wind tunnel test of a 14 percent thick oblique wing

    Kennelly, Robert A., Jr. / Kroo, Ilan M. / Strong, James M. et al. | NTRS | 1990


    Transonic Wind Tunnel Test of Wing Oscillating in Pitch

    Begnini, Guilherme R. / Bones, Carlos A. / Spode, Cleber | AIAA | 2018


    NACA Transonic Wing-tunnel Test Sections

    Wright, Ray H / Ward, Vernon G | NTRS | 1948


    Computational optimization and wind tunnel test of transonic wing designs

    Haney, H.P. / Johnson, R.R. / Hicks, R.M. | Tema Archiv | 1979