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Wind-Tunnel Investigation at High and Low Subsonic Mach Numbers of a Thin Sweptback Wing Having an Airfoil Section Designed for High Maximum Lift
Author:
Racisz, Stanley F.
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L51L04
Link:
https://digital.library.unt.edu/ark:/67531/metadc59896/
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