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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