Pressure Distributions on Plug- and Semaphore-Type Spoiler Ailerons on a 35 Degree Sweptback Wing of Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Section at High Subsonic Speeds

Author: Hammond, Alexander D.
Year: 1954
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L54F08
Link: https://digital.library.unt.edu/ark:/67531/metadc60410/

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