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Showing 10 out of a total of 367 results for collection: Aeronautical Research Council Reports & Memoranda. (0.184 seconds)

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A comparison of results in the A.R.A. transonic tunnel on a small and a large model of a slender wing

T. E. B. Bateman; A. B. Haines (1961)
Calculation of the turbulent boundary layer in a vortex diffuser

T-S Cham; M. R. Head (1969)
A study of the effect of leading-edge modifications on the flow over a 50-deg sweptback wing at transonic speeds

E. W. E. Rogers; C. J. Berry; J. E. G. Townsend (1960)
A numerical method for calculating the pressure due to thickness on symmetrical wings at zero incidence in supersonic flow

R. H. Eldridge; F. Walkden (1966)
Wind-Tunnel Experiments on the Flow over Rectangular Cavities at Subsonic and Transonic Speeds

J. E. Rossiter (1964)
Measurement of the yawing moment and product of inertia of an aircraft by the single point suspension method theory and rig design

A.A. Woodfield (1968)
Tip-clearance flow and losses for an isolated compressor blade

B. Lakshminarayana; J. H. Horlock (1962)
On obtaining solutions to the navier-stokes equations with automatic digital computers

D.B. Russell (1962)
An experiment on aerodynamic nozzles at M = 2

J. Reid (1962)
Estimation of heat transfer to flat plates, cones and blunt bodies

L. F. Crabtree; R. L. Dommett; J. G. Woodley (1965)

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