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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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