NASA-N69-14762

Wind tunnel investigations of vortex breakdown on slender sharp-edged wings

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T16:52:28Z
date available	2017-09-04T16:52:28Z
date copyright	01/01/1968
date issued	1968
identifier other	WTFNKEAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/116007
description abstract	Systematic wind tunnel investigations of vortex breakdown have been conducted on sharp-edged delta and modified delta wings with sweep angles from 45° to 85⁰ at Reynolds numbers of about 1 x 10⁶, utilizing a schlieren system for flow visualization. Vortex breakdown positions are presented as a function of angle of attack and seep. Results agree well with the limited amount of previously published data For the very slender wings (75⁰ to 85⁰ sweep), initial breakdown was nearly independent of sweep, a result not anticipated by extrapolation of previous data.
language	English
title	NASA-N69-14762	num
title	Wind tunnel investigations of vortex breakdown on slender sharp-edged wings	en
type	standard
page	123
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1968
contenttype	fulltext