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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