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 North East Coast Instn Engrs and Shipbldrs -- Trans v 56 pt 5 Mar 1940 p 171-220 and (discussion) pt 7 May-June 1940 p D91-112; Gas and Oil Power (Annual Tech Rev No) 1940 p 240-4 and 232)
Application of two-stroke heavy-oil engine to aircraft propulsion
Automobile Engr
Automobile Engineer ; 30 , n 397 ; p 153-155
1940
3 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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