1–15 von 15 Ergebnissen
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    Preliminary measurements in a shock tunnel of shock angle and undersurface pressure to a Nonweiler wing

    Pennelegion, L. / Cash, R. F. / Aeronautical Research Council | TIBKAT | 1963

    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

    Observations of the flow over a two-dimensional 4 per cent aerofoil at transonic speeds

    Hendshall, B. D. / Cash, R. F. / Aeronautical Research Council | TIBKAT | 1961

    Flow past circular cylinders : simulation of full-scale flows at model scale

    Pearcey, H. H. / Cash, R. F. / Salter, I. J. | TIBKAT | 1982

    An experimental investigation of leading-edge flow separation from a 4 per cent thick two-dimensional biconvex aerofoil

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

    Tests at high subsonic speeds on a 10 per cent thick pressure-plotting aerofoil of RAE 104 section

    Rogers, E. W. E. / Berry, C. J. / Cash, R. F. et al. | TIBKAT | 1956

    Observations of the flow over a two-dimensional 4 per cent thick aerofoil at transonic speeds

    Henshall, B. D. / Cash, R. F. | SLUB | 1961
    Beteiligte: Cash, R. F.

    An experimental investigation of leading-edge flow separation from a 4 per cent thick two-dimensional biconvex aerofoil

    Großbritannien, Aeronautical Research Council | SLUB | 1958
    Beteiligte: Cash, R. F.

    Tests at high subsonic speeds on a 10 per cent thick pressure plotting aerofoil of RAE 104 section

    Rogers, E. W. E. / Berry, C. J. / Cash, R. F. | SLUB | 1956
    Beteiligte: Cash, R. F.