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Experimental and calculated characteristics of three wings of NACA 64-210 and 65-210 airfoil sections with and without 2 degree washout
Author:
Sivells, James C.
Year:
1947
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-1422
Link:
https://digital.library.unt.edu/ark:/67531/metadc54307/
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