Full-Scale Investigation of a Wing With the Leading Edge Swept Back 47.5 Degrees and Having Circular-Arc and Finite-Trailing-Edge-Thickness Ailerons

Author: Lange, Roy H.
Year: 1949
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L9B02
Link: https://digital.library.unt.edu/ark:/67531/metadc58272/

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