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Investigation of Operating Pressure Ratio of a Supersonic Wind Tunnel Utilizing Distributed Boundary-Layer Suction in Test Section
Author:
Cohen, C. B.
Year:
1950
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E50H04
Link:
https://digital.library.unt.edu/ark:/67531/metadc58600/
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