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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