Free-flight Investigation at Transonic Speeds of Drag Coefficients of a Boattail Body of Revolution with a Simulated Turbojet Exhaust Issuing at the Base from Conical Short-length Ejectors
1956-12-13
Miscellaneous
No indication
English
Engineering Index Backfile | 1953
|Effect of exhaust-nozzle ejectors on turbojet noise generation
Engineering Index Backfile | 1955
|On boattail bodies revolution having minimum wave drag
NTRS | 1955
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