Effect of Mach Number on Boundary-Layer Transition in the Presence of Pressure Rise and Surface Roughness on an Ogive-Cylinder Body with Cold Wall Conditions

Author: Carros, Robert J.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A56B15
Link: https://digital.library.unt.edu/ark:/67531/metadc62833/

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