NACA-TR-548

Effect of tip shape and dihedral on lateral-stability characteristics

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T16:51:56Z
date available	2017-09-04T16:51:56Z
date copyright	01/01/1937
date issued	1937
identifier other	WRWUYDAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std/handle/yse/115525
description abstract	This report presents the results of wind tunnel tests to determine the effect of wing-tip shape and dihedral on some of the aerodynamic characteristics of Clark Y wings that affect the performance and lateral stability of airplanes. Force tests at several angles of yaw and rotation tests at zero yaw were made. From these tests the rates of change of rolling moment, yawing moment, and cross-wind force coefficients with angle of yaw and the rate of change of rolling moment coefficient with rolling were determined.
language	English
title	NACA-TR-548	num
title	Effect of tip shape and dihedral on lateral-stability characteristics	en
type	standard
page	10
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1937
contenttype	fulltext