Investigation of a 42.7 degree sweptback wing model to determine the effects of trailing-edge thickness on the aileron hinge-moment and flutter characteristics at transonic speeds
Description: Report presenting an investigation in the high-speed tunnel of a 42.7 degree sweptback wing model to determine the effects of aileron trailing-edge thickness on aileron hinge moments and one-degree-of-freedom aileron flutter. Results regarding the hinge-moment characteristics and free-floating characteristics are also provided.
Date: December 26, 1950
Creator: Thompson, Robert F.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department