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)


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    Title :

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


    Additional title:

    North East Coast Instn Engrs Shipbldrs -- Trans


    Contributors:
    Burn, W.S. (author)


    Publication date :

    1940


    Size :

    50 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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