NACA-TR-1042

Some effects of nonlinear variation in the directional-stability and damping-in-yawing derivatives on the lateral stability of an airplane

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T17:00:20Z
date available	2017-09-04T17:00:20Z
date copyright	01/01/1951
date issued	1951
identifier other	BXDZYDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/123780
description abstract	A theoretical investigation has been made to determine the effect of nonlinear stability derivatives on the lateral stability of an airplane. Motions were calculated on the assumption that the directional-stability and the damping-in-yawing derivatives are functions of the angle of sideslip. The application of the Laplace transform to the calculation of an airplane motion when certain types of nonlinear derivatives are present is described in detail. The types of nonlinearities assumed correspond to the condition in which the values of the directional-stability and damping-in-yawing derivatives are zero for small angle of sideslip.
language	English
title	NACA-TR-1042	num
title	Some effects of nonlinear variation in the directional-stability and damping-in-yawing derivatives on the lateral stability of an airplane	en
type	standard
page	9
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1951
contenttype	fulltext