NACA-TM-X-1665

Effect of large sideslip angles on stability characteristics of a T-tail transport configuration

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:58:44Z
date available	2017-09-04T15:58:44Z
date copyright	01/01/1968
date issued	1968
identifier other	RDNKAEAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/61873
description abstract	Sideslip angle effects on static stability characteristics of T tail transport configuration
language	English
title	NACA-TM-X-1665	num
title	Effect of large sideslip angles on stability characteristics of a T-tail transport configuration	en
type	standard
page	49
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1968
contenttype	fulltext
subject keywords	AERODYNAMIC
subject keywords	AIRCRAFT
subject keywords	ANGLE
subject keywords	ATTACK
subject keywords	CHARACTERISTICS
subject keywords	COEFFICIENTS
subject keywords	CONFIGURATIONS
subject keywords	MOMENTS
subject keywords	SIDESLIP
subject keywords	STABILITY
subject keywords	STATIC
subject keywords	SURFACES
subject keywords	TAIL
subject keywords	TRANSPORT
subject keywords	YAWING