Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil

Author: Bird, J. D.
Year: 1945
Document Type: N/A
Series: NACA Wartime Reports
Report Number: NACA-WR-L-172, NACA-ACR-L5F13a
Link: https://digital.library.unt.edu/ark:/67531/metadc61639/

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