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A correlation of experimental zero-lift drag of rectangular wings with symmetrical NACA 65-series airfoil sections by means of the transonic similarity law for wings of finite aspect ratio
Author:
Danforth, Edward C. B.
Year:
1951
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L51G20
Link:
https://digital.library.unt.edu/ark:/67531/metadc58849/
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