Design and development of supersonic research aircraft, with delta wing plan form of aspect ratio 2, having Rolls-Royce "RA5" engine in body; design matters of interest are: drooping nose, main undercarriage, engine installation, hydraulics and power controls; manufacturing problems. From lecture before Roy Aeronautical Soc. (See also Engineer v 203 n 5274 Feb 22 1957 p 297-9; Flight v 71 n 2509, 2510 Feb 22 1957 p 235-7, Mar 1 p 266-7)
Fairey "Delta 2"
Shell Aviation News
Shell Aviation News ; n 228
1957
4 pages
Article (Journal)
English
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