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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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