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Force and Moment Coefficients for a Thin Airfoil With Flap and Tab in a Form Useful for Stability and Control Calculations
Author:
White, Roland J.
Year:
1945
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-960
Link:
https://digital.library.unt.edu/ark:/67531/metadc54927/
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