1–13 von 13 Ergebnissen
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    Lift-Curve Slope at Subsonic and Supersonic Speeds

    Graphical Presentation of Theoretical Results for Straight-Tapered Wings
    Stanbrook, A. | Emerald Group Publishing | 1954

    Lift-curve slope at subsonic and supersonic speeds

    Stanbrook, A. | Engineering Index Backfile | 1954

    Nozzle and contraction shapes of the R.A.E. 3ft. x 3ft. supersonic wind tunnel

    Stanbrook, A. / Aeronautical Research Council | TIBKAT | 1957

    The flow upstream of finite span spoilers at supersonic speeds

    Stanbrook, A. / Aeronautical Research Council | TIBKAT | 1959

    Experimental observation of vortices in wing-body junctions

    Stanbrook, A. / Aeronautical Research Council | TIBKAT | 1959

    The influence of a model on plenum chamber indication of Mach number in a slotted wall wind tunnel

    Squire, L. C. / Stanbrook, A. / Aeronautical Research Council | TIBKAT | 1958

    Experimental observation of vortices in wing body junctions

    Stanbrook, A. | SLUB | 1959
    Beteiligte: Stanbrook, A.

    An experimental investigation of the characteristics of some plane and cambered 65o delta wings at Mach numbers from 0.7 to 2.0

    Squire, Leonard C. / Jones, J. G. / Stanbrook, A. | SLUB | 1963
    Beteiligte: Stanbrook, A.

    Performance of the 36 x 35 in. slotted transonic working section of the R.A.E. Bedford 3-ft wind tunnel

    Sutton, E. P. / Caiger, M. T. / Stanbrook, A. | SLUB | 1961
    Beteiligte: Stanbrook, A.