1–20 von 549 Ergebnissen
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    Investigating the shock buffet development and spanwise features on an OAT15A profile using background-oriented schlieren

    Freier Zugriff
    Accorinti, Alessandro / Universität der Bundeswehr München, Fakultät für Luft- und Raumfahrttechnik | TIBKAT | 2023

    Wing theory in supersonic flow

    Carafoli, Elie | TIBKAT | 1969

    Some exploratory measurements of leading-edge vortex positions on a delta wing oscillating in heave

    Maltby, R. L. / Engler, P. B. / Keating, R. F. A. et al. | TIBKAT | 1965

    Design of warped slender wings with the attachment line along the leading edge

    Weber, J. / Aeronautical Research Council | TIBKAT | 1965

    The comparison of theory and experiment for oscillating wings

    Acum, W. E. A. / Aeronautical Research Council | TIBKAT | 1963

    Turbulent boundary layers on delta wings at zero lift

    Cooke, J. C. / Aeronautical Research Council | TIBKAT | 1963

    Boundary layer characteristics of Caret wings

    Catherall, D. / Aeronautical Research Council | TIBKAT | 1963

    Surface oil-flow patterns on wings of different leading-edge radius and sweepback

    Garner, H. C. / Cox, D. K. / Aeronautical Research Council | TIBKAT | 1962

    The leading-edge buckling of a thin built-up wing due to aerodynamic heating

    McKenzie, K. I. / Aeronautical Research Council | TIBKAT | 1962

    Calculations of the lift slope and aerodynamic centre of cropped delta wings at supersonic speeds

    Smith, J. H. B. / Beasley, J. A. / Stevens, A. et al. | TIBKAT | 1961

    The calculation of lift slopes, allowing for boundary layer, with applications to the RAE 101 and 104 aerofoils

    Spence, D. A. / Beasley, J. A. / Aeronautical Research Council | TIBKAT | 1960

    Tables of aerodynamic flutter derivatives for thin wings and control surfaces in two dimensional supersonic flow

    Minhinnick, I. T. / Woodcock, D. L. / Aeronautical Research Council | TIBKAT | 1958

    Supersonic wind-tunnel flutter tests of two rectangular wings

    Guyett, P. R. / Aeronautical Research Council | TIBKAT | 1958