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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