NACA-TR-675

Effects of elevator nose shape, gap, balance, and tabs on the aerodynamic characteristics of a horizontal tail surface

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:12:00Z
date available	2017-09-04T15:12:00Z
date copyright	01/01/1939
date issued	1939
identifier other	LVWUYDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/10424
description abstract	Results are presented showing the effects of gap, elevator, nose shape, balance, cut-out, and tabs on the aerodynamic characteristics of a horizontal tail surface tested in the NACA full-scale tunnel.
language	English
title	NACA-TR-675	num
title	Effects of elevator nose shape, gap, balance, and tabs on the aerodynamic characteristics of a horizontal tail surface	en
type	standard
page	11
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1939
contenttype	fulltext