Foremost among difficulties encountered in development of Diesel aircraft engine is requirement of high speed and light weight; account of how this difficulty has been met; examples of early Junkers design; history and performance of 650-hp. 2-cycle engine; fuel injection and scavenging systems; vibration tests; details of present design. (See also - no. 1, Jan. 10, 1930, pp. 2-5; Zeit. fuer Flugtechnik und Motorluftschiffahrt vol. 20, no. 22, Nov. 28, 1929 pp. 578-579, 27 figs.; Nat. Advisory Committee for Aeronautics -- Tech. Memo., no. 565, May 1930, 20 pp., 20 figs.)


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    Title :

    Development of the junkers-diesel aircraft engine


    Additional title:

    Automobiltechnische Zeit


    Contributors:

    Published in:

    Publication date :

    1930


    Size :

    6 pages


    Remarks:

    27 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German




    Development of the junkers-diesel aircraft engine

    Gasterstaedt | Engineering Index Backfile | 1929




    Development of the junkers-diesel aircraft engine

    Gasterstaedt | Engineering Index Backfile | 1930


    Junkers develops diesel engine for aircraft use

    Heinze, E.P.A. | Engineering Index Backfile | 1930