NACA-WR-L-710

Determination of the stability and control characteristics of airplanes from tests of powered models

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:54:39Z
date available	2017-09-04T15:54:39Z
date copyright	01/01/1942
date issued	1942
identifier other	QTCZYDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/58074
description abstract	A technique of testing wind-tunnel powered models has been developed as a result of experience gained in the investigation of the static longitudinal and lateral-stability and control characteristics of several powered models in the NACA 7- by 10-foot wind tunnel. As an important part of this technique, a minimum program of the tests considered necessary to specify satisfactorily the static stability and control characteristics for present-day airplanes has been tentatively established. A discussion of the conditions to be investigated, methods of presenting and interpreting the data, and a suggested operating technique are given. Typical test data, illustrating some of the effects of power on the characteristics of a model of a low-wing single-engine airplane, are also presented.
language	English
title	NACA-WR-L-710	num
title	Determination of the stability and control characteristics of airplanes from tests of powered models	en
type	standard
page	79
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1942
contenttype	fulltext