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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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