The High-Speed Aerodynamic Effects of Modifications to the Wing and Wing-Fuselage Intersection of an Airplane Model with the Wing Swept Back 35 Degrees

Author: Boddy, Lee E.
Year: 1948
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A7J02
Link: https://digital.library.unt.edu/ark:/67531/metadc58169/

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