NASA-TM-X-3087

Lateral-directional stability characteristics of a wing-fuselage configuration at angles of attack up to 44 degrees

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T18:41:31Z
date available	2017-09-04T18:41:31Z
date copyright	01/01/1974
date issued	1974
identifier other	JXITDEAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;query=autho54037D839D40527361598F1ED52F014A/handle/yse/223068
description abstract	An investigation has been conducted to determine the effects of configuration variables on the lateral-directional stability characteristics of a wing-fuselage configuration. The variables under study included variations in the location of a single center-line vertical tail and twin vertical tails, wing height, fuselage strakes, and horizontal tails. The study was conducted in the Langley high-speed 7-by 10-foot tunnel at a Mach number of 0.30, at angles of attack up to 44 deg and at sideslip angles of 0 deg and plus or minus 5 deg.
language	English
title	NASA-TM-X-3087	num
title	Lateral-directional stability characteristics of a wing-fuselage configuration at angles of attack up to 44 degrees	en
type	standard
page	37
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1974
contenttype	fulltext
subject keywords	AERODYNAMIC
subject keywords	AIRCRAFT
subject keywords	BODY
subject keywords	CHARACTERISTICS
subject keywords	CONFIGURATIONS
subject keywords	DIRECTIONAL
subject keywords	LATERAL
subject keywords	SPEED
subject keywords	STABILITY
subject keywords	SUBSONIC
subject keywords	TESTS
subject keywords	TUNNEL
subject keywords	WIND
subject keywords	WING