Engine developed by D.Napier and Son, derivative of which is to power Fairey Rotodyne helicopter, develops at takeoff 3000 ehp for net dry weight of 1575 lb and frontal area of 7.1 sq ft, with specific fuel consumption of 0.624 lb per ehp per hr; performance data; illustrations. (See also Engineering v 178 n 4617 July 23 1954 p 121-123; Flight v 66 n 2374 July 23 1954 p 113-8; Engineer v 198 n 5139 July 23 1954 p 115-8)
"Eland" turbo-propeller engine
Aeroplane
Aeroplane ; 87 , n 2244
1954
7 pages
Aufsatz (Zeitschrift)
Englisch
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"Eland" turbo-propeller engine
Engineering Index Backfile | 1954
"Eland" turbo-propeller engine
Engineering Index Backfile | 1954
"Eland" turbo-propeller engine
Engineering Index Backfile | 1954
Engineering Index Backfile | 1955
|Engineering Index Backfile | 1955
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