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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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