Official report from Ministry of Aircraft Production on bench tests made of Junkers Jumo 211 fuel injection aircraft engine; take-off power 1160 bhp at 2400 rpm and 4.7 lb/sq in. boost.
Type-testing Jumo 211D
Flight
Flight ; 44 , n 1806
1943
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1940
|SLUB | 1944
|SAE Technical Papers | 1946
|Engineering Index Backfile | 1943
Engineering Index Backfile | 1943