Force and moment coefficients for a thin airfoil with flap and tab in a form useful for stability and control calculations

White, Roland J (Curtiss-Wright Corporation) Klampe, Dean G (Curtiss-Wright Corporation)
naca-tn-960
1945


No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1945/naca-tn-960.pdf