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)


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    Title :

    Application of two-stroke heavy-oil engine to aircraft propulsion


    Additional title:

    Automobile Engr


    Contributors:
    Burn, W.S. (author)

    Published in:

    Automobile Engineer ; 30 , n 397 ; p 153-155


    Publication date :

    1940


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Application of two-stroke heavy-oil engine to aircraft propulsion

    Burn, W.S. | Engineering Index Backfile | 1940


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