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.)
Development of the junkers-diesel aircraft engine
Automobiltechnische Zeit
Automobiltechnische Zeitschrift ; 33 , n 2
1930
6 pages
27 Figs.
Article (Journal)
German
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Development of the junkers-diesel aircraft engine
Engineering Index Backfile | 1929
|Development of the Junkers-diesel Aircraft Engine
NTRS | 1930
|Development of the Junkers Diesel aircraft engine
SLUB | 1930
|Development of the junkers-diesel aircraft engine
Engineering Index Backfile | 1930
|Junkers develops diesel engine for aircraft use
Engineering Index Backfile | 1930
|