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Low-Speed Investigation of the Effects of Wing Tanks and Speed Brakes on the Static Stability of a Model Having a 40 Degree Swept Wing
Author:
Sleeman, William C., Jr.
Year:
1955
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L55C17
Link:
https://digital.library.unt.edu/ark:/67531/metadc61216/
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