Pressure Distribution and Damping in Steady Roll at Supersonic Mach Numbers of Flat Swept-Back Wing with Subsonic Edges

Author: Walker, Harold J.
Year: 1950
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-2047
Link: https://digital.library.unt.edu/ark:/67531/metadc55372/

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