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Showing 10 out of a total of 74 results for community: Aeronautical Research Council. (0.097 seconds)

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The influence of a wide hub on the room temperature burst strength of model steam turbine rotors

N. E. Waldren; D. E. Ward (1963)
Preliminary measurements in a shock tunnel of shock angle and undersurface pressure related to a nonweiler wing

L. Pennelegion; R. F. Cash (1963)
A preliminary study of ionic recombination of argon in wind-tunnel nozzles part 2

K. N. C. Bray; J. A. Wilson (1963)
The pressure calibration of the R.A.E. 6 inch diameter shock tube with a view to its use as the driver of a cold high-density hypersonic tunnel

S. G. Cox; R. J. Pallant; J. M. Shaw (1963)
Tunnel tests on a double cascade to determine the interaction between the rotor and the nozzles of a supersonic turbine

B. S. Stratford; G. E. Sansome (1963)
A theoretical investigation of the effect of change in axial velocity on the potential flow through a cascade of aerofoils

D. Pollard; J. H. Horlock (1963)
On the effect of fan and thrust engine loading on the transition power requirements of a fan wing

N. Gregory (1963)
On Three-Dimensional Bodies of Delta Planform which can Support Plane Attached Shock Waves

D. H. Peckham (1963)
The boundary layer drag of bodies with swept trailing edges in supersonic flow

J. C. Cooke (1963)
Propagation of fatigue cracks in wide unstiffened aluminium alloy sheets

K.D. Raithby; Marie E. Bebb (1963)

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- 1963 (74)