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Showing 10 out of a total of 105 results for community: Aeronautical Research Council. (0.12 seconds)

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Wind tunnel force and moment investigation at M = 4.3 into the application of various devices for the control of a cone-cylinder-flare configuration

B. E. Pecover (1964)
Power spectra of low level atmospheric turbulence measured from an aircraft

A. Burns (1964)
Wind tunnel tests at M = 2.0 on interference effects between intake flows in a four-engine nacelle

M. D. Dobson (1964)
Some tests with trapped vortices in supersonic flow

B. S. Stratford; M. C. Neale (1964)
Some notes on turbulent boundary layers with fluid injection at high supersonic speeds

L. C. Squire (1964)
Pressure, heat transfer and temperature measurements in the two-dimensional nozzle of a reflected-shock tunnel

J. L. Stollery; J. E. G. Townsend (1964)
A free-flight investigation of wing-body junction design for a transonic swept-wing aircraft

G. K. Hunt (1964)
Flutter tests and calculations on an all-moving model fin

J. K. Curran (1964)
Use of a wind tunnel to determine the performance of slender wings suitable for a supersonic transport aircraft

J. Y. G. Evans (1964)
A theoretical approach to air bag shock absorber design

A.C. Browning (1964)

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- 1964 (105)