Case for heavy oil airplane engine and its present position; resume of past developments; special problems of scavenging, port and piston design, cooling, combustion chambers and fuel injection; suggested horizontal opposed piston, airplane engine design by author, which complies with greatest number of aeronautic requirements and is yet basically efficient. (See also - (discussion) pt 7 May-June 1940 p D91-112; Automobile Engr v 30 n 397 May 1940 p 153-5; Gas and Oil Power (Annual Tech Rev No) 1940 p 240-4 and 232)
Application of two-stroke heavy-oil engine to aircraft propulsion
North East Coast Instn Engrs Shipbldrs -- Trans
North-East Coast Institution of Engineers and Shipbuilders -- Transactions ; 56 , Part 5 ; p 171-220
1940
50 pages
Aufsatz (Zeitschrift)
Englisch
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Application of two-stroke heavy-oil engine to aircraft propulsion
Engineering Index Backfile | 1940
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