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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