Details released by D.Napier and Son of "Nomad", oa compression ratio of 31.5:1 and expansion ratio of 24:1 is achieved, leading to fuel consumption in order of 0. 35 lb per bhp-hr; total power developed in gas turbine alone is 2250 hp and in diesel engine alone 2660 hp. See also Engineering Index 1953 p 41. (See also Engineer v 197 n 5127 Apr 30 1954 p 637-640; Engineering v 177 n 4604 Apr 30 1954 p 571-572; Oil Engine and Gas Turbine v 22 n 251 May 1954 p 18-20; Gas and Oil Power v 49 n 587 May 1954 p 101-4; Aviation Week v 60 n 20 May 17 1954 p 30-2, 34; English Elec J v 13 n 7 Sept 1954 p 295-302)
Aeronautical compound diesel engine
Flight
Flight ; 65 , n 2362
1954
9 pages
Article (Journal)
English
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Aeronautical compound diesel engine
Engineering Index Backfile | 1954
Aeronautical compound diesel engine
Engineering Index Backfile | 1954
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