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Effects of Rocket-Armament Exhaust Gas on the Performance of a Supersonic-Inlet J34-Turbojet-Engine Installation at Mach 2.0
Author:
Beheim, Milton A.
Year:
1956
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E55K22
Link:
https://digital.library.unt.edu/ark:/67531/metadc62417/
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