NACA-TR-1304

Flight investigation of the effectiveness of an automatic aileron trim control device for personal airplanes

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T17:29:41Z
date available	2017-09-04T17:29:41Z
date copyright	01/01/1957
date issued	1957
identifier other	CSUYYDAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std/handle/yse/152743
description abstract	A flight investigation to determine the effectiveness of an automatic aileron trim control device installed in a personal airplane to augment the apparent spiral stability has been conducted. The device utilizes a rate-gyro sensing element in order to switch an on-off type of control that operates the ailerons at a fixed rate through control centering springs. An analytical study using phase-plane and analog-computer methods has been carried out to determine a desirable method of operation for the automatic trim control.
language	English
title	NACA-TR-1304	num
title	Flight investigation of the effectiveness of an automatic aileron trim control device for personal airplanes	en
type	standard
page	16
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1957
contenttype	fulltext