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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