Browsing Aeronautical Research Council Reports & Memoranda by Author "A. L. Courtney"

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10-ft x 7-ft tunnel tests up to M = 0.94 of nose droop and a blunt-nosed NACA 3-00 type section on a 7.5 per cent thick 50 deg swept wing

A. L. Courtney (1958)

This note describes further tests made during 1954 in the Royal Aircraft Establishment 10 ft x 7 ft High Speed Tunnel, as part of a research programme to improve the subsonic longitudinal stability characteristics of a 50 ...
Pressure-plotting and force tests at mach numbers up to 2.8 on an uncambered slender wing of p = .50, S/Co = .25 'handley page ogee'

A. L. Courtney; A. O. Ormerod (1961)

Pressure-plotting and force tests have been made in the 8 ft x 8 ft Wind Tunnel, Bedford, on an uncambered slender wing of Collingbourne p = ½ ogee planform, s/c o = 0.25, 'Newby' area distribution, and varying cross-section ...

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