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 Zeit. fuer Flugtechnik und Motorluftschiffahrt vol. 20, no. 22, Nov. 28, 1929 pp. 578-579, 27 figs,; Automobiltechnische Zeit., vol. 33, nos. 1 and 2, Jan. 10, 1930, pp. 2-5 and Jan. 20, pp. 41-46, 27 figs.)
Development of the junkers-diesel aircraft engine
Nat. Advisory Committee Aeronautics -- Tech. Memo
1930
20 pages
20 Figs.
Report
Englisch
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Development of the Junkers Diesel aircraft engine
SLUB | 1930
|Development of the junkers-diesel aircraft engine
Engineering Index Backfile | 1930
|Development of the junkers-diesel aircraft engine
Engineering Index Backfile | 1929
|Junkers develops diesel engine for aircraft use
Engineering Index Backfile | 1930
|Junkers develops an aircraft diesel
Engineering Index Backfile | 1930
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