NACA-TN-2340

A survey of methods for determining stability parameters of an airplane from dynamic flight measurements

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T18:32:32Z
date available	2017-09-04T18:32:32Z
date copyright	01/01/1951
date issued	1951
identifier other	JBKUYDAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;query=author:%22NAVY%20-%206159DD6E273C9FCD0Facil/handle/yse/214666
description abstract	Various methods of reducing to stability parameter form the response to sinusoidal and transient disturbances are discussed, using the simplified longitudinal motion of an idealized airplane as an illustrative example. It is shown that there are basic limitations in the determination of some of the stability derivatives as compared with the transfer-function coefficients, which are certain combinations of stability derivatives directly related to the airplane response. Hence, most of the report is concerned with methods of determining transfer-function coefficients rather than stability derivatives.
language	English
title	NACA-TN-2340	num
title	A survey of methods for determining stability parameters of an airplane from dynamic flight measurements	en
type	standard
page	52
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1951
contenttype	fulltext