Wind-tunnel investigation at low speed of the lateral control characteristics of ailerons having three spans and three trailing-edge angles on a semispan wing model

Leslie E. Schneiter, Rodger L. Naeseth
naca-tn-1738
Nov 1948


A wind-tunnel investigation has been made of the low-speed lateral control characteristics of a tapered, low-drag, semispan wing model equiped with 20-percent-chord sealed ailerons having spans of 0.954, 0.583, and 0.294 percent of a full-span aileron, each with trailing-edge angles of 6, 14, and 25 degrees.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1948/naca-tn-1738.pdf