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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