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Investigation to Mach number 2.0 of shock-positioning control systems for a variable-geometry inlet in combination with a J34 turbojet engine
Author:
Leissler, L Abbott
Year:
1954
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E54I27
Link:
https://digital.library.unt.edu/ark:/67531/metadc60938/
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