NACA-TR-823

Experimental verification of a simplified vee-tail theory and analysis of available data on complete models with vee tails

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:12:56Z
date available	2017-09-04T15:12:56Z
date copyright	01/01/1945
date issued	1945
identifier other	LYWUYDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/11537
description abstract	An analysis has been made of available data on vee tail surfaces. Previously published theoretical studies of vee tails have been extended to include the control effectiveness and control forces in addition to the stability. Tests of two isolated tail surfaces with various amounts of dihedral provided a check of the theory. Methods for designing vee tails were also developed and are given in the present paper.
language	English
title	NACA-TR-823	num
title	Experimental verification of a simplified vee-tail theory and analysis of available data on complete models with vee tails	en
type	standard
page	21
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1945
contenttype	fulltext
subject keywords	AERODYNAMIC
subject keywords	AIRCRAFT
subject keywords	CHARACTERISTICS
subject keywords	CONTROL
subject keywords	DESIGN
subject keywords	SPIN
subject keywords	STABILITY