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Investigation at high and low subsonic Mach numbers of two symmetrical 6-percent-thick airfoil sections designed to have high maximum lift coefficients at low speeds
Author:
Paradiso, Nicholas J.
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L52I02
Link:
https://digital.library.unt.edu/ark:/67531/metadc59367/
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