Investigation of Low-Speed Aileron Control Characteristics at a Reynolds Number of 6,800,000 of a Wing With Leading Edge Swept Back 42 Degrees With and Without High-Lift Devices

Author: Bollech, Thomas V.
Year: 1949
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L9E24
Link: https://digital.library.unt.edu/ark:/67531/metadc58343/

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