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A method of estimating the aerodynamic effects of ordinary and split flaps of airfoils similar to the Clark Y
Author:
Pearson, H. A.
Year:
1936
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-571
Link:
https://digital.library.unt.edu/ark:/67531/metadc54206/
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