Internal performance of several auxiliary air inlets immersed in a turbulent boundary layer at Mach numbers of 1.3, 1.5, and 2.0

Author: Huff, Ronald G.
Year: 1957
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E56J18
Link: https://digital.library.unt.edu/ark:/67531/metadc62998/

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