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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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