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Approximate Method for Calculation of Laminar Boundary Layer With Heat Transfer on a Cone at Large Angle of Attack in Supersonic Flow
Author:
Brunk, William E.
Year:
1958
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-4380
Link:
https://digital.library.unt.edu/ark:/67531/metadc57536/
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