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Showing 10 out of a total of 313 results for collection: Aeronautical Research Council Reports & Memoranda. (0.117 seconds)

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Photographs of shock wave movement

W. F. Hilton; R. G. Fowler (1947)
Wind-tunnel tests on the spoiling effects of engine cooling gills on radial air-cooled installations on a wing

J. Seddon; J. A. Kirk (1942)
Flight tests at high mach number on E28/39 W4041 (single-engined jet-propelled aircraft)

A. W. Thom; F. Smith; J. Brotherton (1945)
High-speed tunnel tests of a 5 per cent. Chord dive-recovery flap on a NACA 0015 aerofoil

D. A. Clarke (1948)
Wing parachutes for recovery from the spin. Part I - General design requirements. Part II - Wake Phenomena.

G. E. Pringle; T. V. Somerville; D. J. Harper; J. R. Mitchell; J. Picken; G. E. Pringle (1947)
The high-speed laboratory of the aerodynamics Division, N.P.L. Part I - description of the installation. Part II - experimental techniques. Part III - experimental results.

D. W. Holder (1946)
Low-speed measurements of the pressure distribution at the surface of a swept-back wing

V. M. Falkner; Doris E. Lehrian (1949)
An aerofoil designed to give laminar flow over the whole surface with boundary-layer suction

E. J. Richards; C. H. Burge (1943)
On the solution of linear simultaneous differential equations with constant coefficients by a process of isolation

J. Morris (1947)
Some wind-tunnel developments of the spoiler as a form of lateral control

W. S. Coleman; G. H. Tidbury (1942)

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