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Showing 10 out of a total of 59 results for community: Aeronautical Research Council. (0.167 seconds)

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Conical flow as a result of shock and boundary-layer interaction on a probe

J. Lukasiewicz (1948)
The indication of boundary-layer transition on aerofoils in the N.P.L. 20 in. x 8 in. high speed wind tunnel

H.H. Pearcey (1948)
Some electrical integrating circuits and their use in the measurement of low frequency vibration amplitudes

G. R. Richards (1948)
The dynamic landing loads of flying boats with special reference to measurements made on Sunderland TX.293

Anne Burns; A. J. Fairclough (1948)
Note on the dynamic characteristics of servo-tab systems of control

D. Adamson; D. J. Lyons (1948)
Regenerator heat exchangers for gas-turbines

J. E. Johnson (1948)
The Flow in an Axially-Symmetric Supersonic Jet from a Nearly-Sonic Orifice into a Vacuum

P. L. Owen; C. K. Thornhill (1948)
Model tests on an air interchange system for removing engine exhaust products from a wind tunnel

K. W. Newby; E. G. Barnes; D. W. Bottle (1948)
Boundary-layer flow along a flat plate with uniform suction

J. M. Kay (1948)
Systematic wind-tunnel tests with slats on a 10 per cent thick symmetrical wing section (EQ 1040 profile)

G. F. Moss (1948)

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- 1948 (59)