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Investigation at a Mach Number of 1.2 of Two 45 Degree Sweptback Wings Utilizing NACA 2-006 and NACA 65A006 Airfoil Sections
Author:
Wilson, Homer B., Jr.
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L52G17
Link:
https://digital.library.unt.edu/ark:/67531/metadc59310/
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