Browsing Aeronautical Research Council by Author "A. C. S. Pindar"

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Balance and pressure measurements at high subsonic speeds on a model of a swept-wing aircraft (Hawker P.1052) and some comparisons with flight data

J. R. Collingbourne; A. C. S. Pindar (1953)

Basic results are given of measurements in the Royal Affcraft Establishment 10-ft × 7-ft Subsonic Wind Tunnel over a range of lift coefficient at Mach numbers up to 0.93, the Reynolds number being 1.75 million. Though a ...
Pressure plotting and balance measurements in the high speed wind tunnel on a half-model of a 90-deg-apex delta wing with fuselage

A. C. S. Pindar; J. R. Collingbourne (1949)

Tests were made at a Reynolds number of 1.8 x 10power6 and Mach numbers up to 0.93. The wing tip was cropped to a taper of 1/7 and the wing section was RAE 102, symmetrical, 10 per cent thickness/chord at 35 per cent chord. ...

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