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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