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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