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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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