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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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