An investigation at low speed of a 51.3 degrees sweptback semispan wing with a raked tip and with 16.7-percent-chord ailerons having three spans and three trailing-edge angles

Author: Schneiter, Leslie E
Year: 1948
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L8F29
Link: https://digital.library.unt.edu/ark:/67531/metadc57806/

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