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Showing 10 out of a total of 40 results for collection: Aeronautical Research Council Reports & Memoranda. (0.189 seconds)

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Concept of complex stiffness applied to problems of oscillations with viscous and hysteretic damping

S. Neumark (1957)
Boundary-layer measurements on 15-deg and 24.5-deg cones at small angles of incidence at M = 3.17 and 3.82 and zero heat transfer

F. V. Davies; R. J. Monaghan (1957)
The design and testing of an axial-flow compressor having different blade profiles in each stage

A. D. S. Carter; R. C. Turner; D. W. Sparkes; R. A. Burrows (1957)
The wave drag of non-lifting combinations of thin wings and 'non-slender' bodies

L. M. Sheppard (1957)
Free vibrations of a stiffened cylindrical shell

P. R. Miller (1957)
An approximate method of calculating the laminar boundary layer in two-dimensional incompressible flow

M. R. Head (1957)
Measurements of the direct hinge-moment derivatives at subsonic and transonic speeds for a cropped delta wing with oscillating flap

J. B. Bratt; C. J. W. Miles; R. F. Johnson (1957)
The formation of regions of separated flow on wing surfaces Part 1 low-speed tests on a two-dimensional unswept wing with a 10 per cent thick RAE 101 section Part 2 laminar-separation bubbles and the mechanism of the leading-edge stall

L. F. Crabtree (1957)
The effect of reynolds number on the performance of a single-stage compressor

A. D. S. Carter; C. E. Moss; G. R. Green; G. G. Annear (1957)
An experimental investigation of leading-edge flow separation from a 4 per cent thick two-dimensional biconvex aerofoil

B. D. Henshall; R. F. Cash (1957)

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- 1957 (40)