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Wind tunnel investigation of NACA 66(215)-216, 66,1-212, and 65(sub 1)-212 airfoils with 0.20-airfoil-chord split flaps
Author:
Fullmer, Felicien F., Jr.
Year:
1944
Document Type:
N/A
Series:
NACA Wartime Reports
Report Number:
NACA-WR-L-140, NACA-CB-L4G10
Link:
https://digital.library.unt.edu/ark:/67531/metadc61376/
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