Simple and accurate calculations are made of the flow process in a continuous compressorless Lorin jet-propulsion unit. Experimental confirmation is given from towing tests on an airplane at flying speeds up to 200 miles per second. An analysis is made of the performance of a fighter-type airplane designed for utilization of this propulsion system.
A Ram-Jet Engine for Fighters
1947-10-01
Miscellaneous
No indication
English
Engineering Index Backfile | 1947
|TIBKAT | 1947
|Engineering Index Backfile | 1930
|Engineering Index Backfile | 1950
Aft-End Design Techniques for Twin-Engine Fighters
AIAA | 1974
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