1–20 von 548 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

    A flexible wing modeling and physical mass estimation system for early aircraft design stages

    Freier Zugriff
    Dorbath, Felix / Technische Universität Hamburg-Harburg, Institut für Lufttransportsysteme | TIBKAT | 2014

    The airforces on the low-aspect-ratio rectangular wing oscillating in sonic flow

    Davies, D. E. / Aeronautical Research Council | TIBKAT | 1963

    Experiments at M=1.41 on a thin, conically-cambered elliptic cone of 30° semi-vertex angle

    Rogers, E. W. E. / Quincey, V. G. / Callinan, J. et al. | TIBKAT | 1963

    Aerodynamic derivative measurements on a wing with a horn-balanced control surface

    Guyett, P. R. / Curran, J. K. / Aeronautical Research Council | TIBKAT | 1963

    Reduction of lift-dependent drag with separated flow

    Lee, G. H. / Aeronautical Research Council | TIBKAT | 1962

    The fatigue strength characteristics of a single spar wing

    Winkworth, W. J. / Aeronautical Research Council | TIBKAT | 1961

    Balance and pressure measurements on wings of different aspect ratios

    Küchemann, D. / Weber, J. / Brebner, G. G. | TIBKAT | 1958

    Observations of the flow past a two-dimensional 4 per cent thick biconvex aerofoil at high subsonic speeds

    Henshall, B. D.H / Cash, R. F. / Aeronautical Research Council | TIBKAT | 1958

    Charts of the theoretical wave drag of wings at zero-lift

    Bishop, R. A. / Cane, E. G. / Aeronautical Research Council | TIBKAT | 1957

    Wind-tunnel wall interference effects on oscillating aerofoils in subsonic flow

    Jones, W. P. / Großbritannien, Aeronautical Research Council | TIBKAT | 1957

    The effects of taper on the supervelocities on three-dimensional wings at zero incidence

    Newby, K. W. / Großbritannien, Aeronautical Research Council | TIBKAT | 1957