1–20 von 116 Ergebnissen
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    Intensiteitsmetingen aan kusntmatige ultravioletlichtbronnen

    Wijk, A. / Reerink, E. H. | TIBKAT | 1933

    Tests on aerofoil flaps in the compressed air tunnel

    Jones, R. / Bell, A. H. / Smyth, E. | TIBKAT | 1935

    Tests of six aerofoil sections at various Reynolds numbers in the compressed air tunnel

    Relf, E. F. / Jones, R. / Bell, A. H. | TIBKAT | 1936

    Tests of four airscrew sections in the compressed air tunnel

    Williams, D. H. / Brown, A. F. / Smyth, E. | TIBKAT | 1936

    Tests of aerofoil N.A.C.A. 23012 in the compressed air tunnel

    Williams, D. H. / Bell, A. H. / Smyth, E. | TIBKAT | 1937

    Bayerische Motor Werke (BMW)

    Liebhafsky, H. A. / Norris, R. H. / Hull, E. H. | TIBKAT | 1945

    Approximate wall corrections for an oscillating swept wing in a wind tunnel of closed circular section

    Acum, W. E. A. / Garner, H. C. / Großbritannien, Aeronautical Research Council | TIBKAT | 1955

    Problems in computation of aerodynamic loading on oscillating lifting surfaces

    Garner, H. C. / Acum, W. E. A. / Aeronautical Research Council | TIBKAT | 1957

    Interference corrections for asymmetrically loaded wings in closed rectangular wind tunnels

    Garner, H. C. / Acum, W. E. A. / Großbritannien, Aeronautical Research Council | TIBKAT | 1957

    Theoretical subsonic derivatives for an oscillating M-wing

    Garner, H. C. / Acum, W. E. A. / Aeronautical Research Council | TIBKAT | 1961

    Comparative calculations of supersonic pitching derivatives over a range of frequency parameter

    Garner, H. C. / Acum, W. E. A. / Lehrian, Doris E. et al. | TIBKAT | 1962

    The estimation of oscillatory wing and control derivatives

    Acum, W. E. A. / Garner, H. C. | TIBKAT | 1964