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Showing 10 out of a total of 47 results for collection: Aeronautical Research Council Reports & Memoranda. (0.185 seconds)

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Internal air-cooling for turbine blades a general design survey

D. G. Ainley (1955)
On some aspects of the use of shock tubes in aerodynamic research

B. D. Henshall (1955)
Some observations of the flow over a delta-winged model with 55-deg leading-edge sweep, at Mach numbers between 0.4 and 1.8

E. P. Sutton (1955)
On the stressing of multi-rib thin wings of low aspect ratio and rectangular plan-form

L. S. D. Morley (1955)
Low-speed-tunnel model tests on the flow structure behind a delta-wing aircraft and a 40 deg swept-wing aircraft at high incidences

D. A. Kirby; A. Spence (1955)
The interaction between shock waves and boundary layers at the trailing edge of a double-wedge aerofoil at supersonic speed

B. D. Henshall; R. F. Cash (1955)
Experiments at M = 1.41 on elliptic cones with supersonic leading edges

E. W. E. Rogers; C. J. Berry (1955)
Effect of Yaw on the compressible laminar boundary layer

J. Tinkler (1955)
Measurements of two-dimensional derivatives on a wing-aileron-tab system with a 1541 section aerofoil. Part 2 direct tab and cross aileron-tab derivatives

K. C. Wight (1955)
A new standard for the prediction of full-scale spin and recovery characteristics from model tests

T. H. Kerr (1955)

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- 1955 (47)