Pressure distributions and force tests of an NACA 65-210 airfoil section with a 50-percent-chord flap

Kelin, Milton M
naca-tn-1167
1947


No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1947/naca-tn-1167.pdf