British Aircraft Corp 221 supersonic research aircraft has been built to explore behavior of slender delta wing at angles of attack high enough to generate powerful vortex above leading edge; background of development and design philosophy applied; problems encountered with regard to intake development; details of fuselage, flying controls, fuel and hydraulic system; communications and instrumentation; power plant is Rolls-Royce Avon RA.28R reheat engine; cutaway drawing.
BAC.221 -- Slender-Delta Research Aircraft
Flight
Flight ; 86 , n 2889
1964
6 pages
Aufsatz (Zeitschrift)
Englisch
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Stability and control of slender delta aircraft
Engineering Index Backfile | 1968
The Stability and Control of Slender Delta Aircraft
Emerald Group Publishing | 1968