NACA-TN-1573

Flight measurements of the flying qualities of five light airplanes

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T18:46:27Z
date available	2017-09-04T18:46:27Z
date copyright	01/01/1948
date issued	1948
identifier other	KJLUYDAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;query=autho182693FD081D206861598F1EFDEC014A/handle/yse/227682
description abstract	Results are presented of an investigation made to determine measurements of stability, controllability, and stalling characteristics of five light airplanes. Comparison of the characteristics of these airplanes with the requirements for satisfactory flying qualities loads to the following conclusions: The five airplanes were stable longitudinally in most of the conditions tested. The degree of stability varied considerably among the five airplanes, but the up-elevator position required to stall with power on was low relative to the maximum deflection of the elevator. The control surfaces of all the airplanes were satisfactorily effective in producing changes in attitude and angular velocity about their respective axes.
language	English
title	NACA-TN-1573	num
title	Flight measurements of the flying qualities of five light airplanes	en
type	standard
page	84
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1948
contenttype	fulltext