Flight measurements of the stability, control, and stalling characteristics of an airplane having a 35 degree sweptback wing without slots and with 80-percent-span slots and a comparison with wind-tunnel data

S. A. Sjoberg, J. P. Reeder
naca-tn-1743
Nov 1948


Flight measurements have been made to determine the low-speed flying qualities of an airplane having a wing swept back 35 degrees at the quarter-chord line. The lateral and directional stability and control characteristics of the airplane without slots and with 80-percent-span slots on the wing are presented.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1948/naca-tn-1743.pdf