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Downwash survey behind two low-aspect-ratio variable-incidence wings in combination with three different size fuselages at a Mach number of 0.25
Author:
Hopkins, Edward J.
Year:
1955
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A55A07
Link:
https://digital.library.unt.edu/ark:/67531/metadc61177/
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