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Showing 10 out of a total of 47 results for collection: Aeronautical Research Council Reports & Memoranda. (0.166 seconds)

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Supersonic flow past quasi-cylindrical bodies of almost circular cross-section

D. G. Randall (1955)
Some factors influencing the speed of response of hydraulic position servomechanisms

C. W. Lewis (1955)
Subsonic wind-tunnel tests on a crescent-winged aircraft, including tests of leading-edge droop designs and several tailplane heights

C. N. Hall; B. J. Prior (1955)
The aerodynamic effects of aspect ratio and sweepback on wing flutter

W. G. Molyneux; H. Hall (1955)
A comparison of the measured and predicted flutter characteristics of a series of delta wings of different aspect ratios

H. Hall; E. W. Chapple (1955)
An experimental investigation of the transonic flow over an unswept wing of aspect ratio 3.5, taper ratio 0.5, with a 4 per cent biconvex section

J. B. Scott-Wilson (1955)
Velocities on two-dimensional closed and semi-infinite aerofoils at zero incidence

S. Neumark; B. Thwaites (1955)
Wind-tunnel tests on seaplane hulls in the R.A.E. 5-ft diameter open jet tunnel and the N.P.L. compressed air tunnel

A. G. Smith (1955)
Experimental and theoretical investigations of the flow of air through two single-stage compressors

J. H. Horlock (1955)
Calculated velocity distribution and force derivatives for a series of high-speed aerofoils

C. S. Sinnott (1955)

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- 1955 (47)