NACA-TN-3176

Wall interference in wind tunnels with slotted and porous boundaries at subsonic speeds

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T18:39:56Z
date available	2017-09-04T18:39:56Z
date copyright	01/01/1954
date issued	1954
identifier other	JTNUYDAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;query=autho162sAF679D40AC421854DD6EFDEC9FCD/handle/yse/221622
description abstract	Linearized compressible-flow analysis is applied to the study of wind-tunnel-wall interference for subsonic flow in either two-dimension or circular test sections having slotted or porous walls. Expressions are developed for evaluating blockage and lift interference.
language	English
title	NACA-TN-3176	num
title	Wall interference in wind tunnels with slotted and porous boundaries at subsonic speeds	en
type	standard
page	43
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1954
contenttype	fulltext