Author : Stewart M. Crandall
Publisher :
Page : 28 pages
File Size : 43,9 MB
Release : 1946
Category : Airplanes
ISBN :
An analysis was made of the hinge-moment effectiveness of tabs based on the available two- and three-dimensional tab data. The results of the analysis indicated that the effects of tabs on control-surface hinge moments can be estimated from geometric characteristics of the tab-flap-airfoil combination with a reasonable degree of accuracy.