Drag Reduction by Suction of the Boundary Layer Separated Behind Shock Wave Formation at High Mach Numbers

Author: Regenscheit, B.
Year: 1947
Document Type: N/A
Series: NACA Technical Memorandums
Report Number: NACA-TM-1168
Link: https://digital.library.unt.edu/ark:/67531/metadc63990/

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