High-speed wind-tunnel investigation of high lift and aileron-control characteristics of an NACA 65-210 semi-span wing

Jack Fischel, Leslie E. Schneiter
naca-tn-1473
Nov 1947


A high-speed wind-tunnel investigation was made of the aerodynamic characteristics at various Mach numbers of an NASA 65-210 semispan wing variously equipped with a 25-percent-chord full-span slotted flap and a 38-percent-semispan 20-percent-chord straight-sided ailaron.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1947/naca-tn-1473.pdf