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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