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An experimental study at moderate and high subsonic speeds of the flow over wings with 30 degrees and 45 degrees of sweepforward in conjunction with a fuselage
Author:
Whitcomb, Richard T
Year:
1951
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L50K28
Link:
https://digital.library.unt.edu/ark:/67531/metadc58701/
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