Concord supersonic transport will be powered by 4 Olympus 593 turbojet engines; Bristol Siddeley will provide turbojets; jet pipe; propulsive nozzles, reversers and silencers are SNECMA contribution; choice of optimum-cycle engine for supersonic aircraft is compromise; maximum thrust is required at takeoff, during transonic acceleration and when cruising; at same time low consumption is essential while cruising and during considerable time at subsonic speeds; development problems involved; Concord flight plan; problems raised by intake and exhaust system.
Concord propulsion
Flight
Flight ; 85 , n 2876
1964
3 pages
Article (Journal)
English
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Engineering Index Backfile | 1964
|Engineering Index Backfile | 1964
|Engineering Index Backfile | 1964
|Emerald Group Publishing | 1964
|Online Contents | 1994