Requirements of thrust reverser to reduce aircraft landing runs; examination of four reverser configurations and reasons for discarding them; basic Rolls-Royce reverser design finally adopted is of sleeve valve and clamshell type; design details of outlet vanes, bearings, pneumatic rams and linkage, etc; bench and flight testing. (see also Flight v 75 n 2611 Feb 6 1959 p 187)
Thrust reversal for jet aircraft
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 63 , n 586
1959
9 pages
Article (Journal)
English
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Thrust reversal for jet aircraft
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