Full-Scale-Wind-Tunnel Tests of a 35 Degree Sweptback Wing Airplane With High-Velocity Blowing Over the Training-Edge Flaps

Author: Kelly, Mark W.
Year: 1955
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A55I09
Link: https://digital.library.unt.edu/ark:/67531/metadc62799/

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