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The effects of high-lift devices on the low-speed stability of a tapered 37.5 degree sweptback wing of aspect ratio 3 in straight and rolling flow
Author:
Queijo, M. J.
Year:
1948
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L8I03
Link:
https://digital.library.unt.edu/ark:/67531/metadc57946/
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