Scale-effect tests in a turbulent tunnel of the NACA 65(sub 3)-418, a = 1.0 airfoil section with 0.20-airfoil-chord split flap Page: 19 of 22
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NACA ACR No. L4122
Fig. 4a, b
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Peyna/ds n ze4 R
/Faure 4 - Sc/ effect on /f/-curve slope of
fte VACA 653-4/8 a/rfo/ second.
COMMITTEE FOR AERONAUTICS.
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Tucker, Warren A. & Wallace, Arthur R. Scale-effect tests in a turbulent tunnel of the NACA 65(sub 3)-418, a = 1.0 airfoil section with 0.20-airfoil-chord split flap, report, September 1944; (digital.library.unt.edu/ark:/67531/metadc61404/m1/19/: accessed October 17, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.