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Tests of three tapered airfoils based on the N.A.C.A. 2200, the N.A.C.A.-M6, and the Clark Y sections
Author:
Anderson, Raymond F.
Year:
1934
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-487
Link:
https://digital.library.unt.edu/ark:/67531/metadc54379/
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