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Boundary-layer transition at Mach 3.12 as affected by cooling and nose blunting
Author:
Diaconis, N S
Additional Authors:
Jack, John R
Year:
1957
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-3928
Link:
https://digital.library.unt.edu/ark:/67531/metadc56706/
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