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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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