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Test of NACA 66,2-116, a = 0.6 airfoil section fitted with pressure balanced and slotted flaps for the wing of the XP-63 airplane
Author:
Abbott, Frank T , Jr
Year:
1942
Document Type:
N/A
Series:
NACA Wartime Reports
Report Number:
NACA-WR-L-701, NACA-MR
Link:
https://digital.library.unt.edu/ark:/67531/metadc61351/
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