NACA-RM-L52B13

Effects of some primary variables of rectangular vortex generators on the static-pressure rise through a short diffuse

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:19:12Z
date available	2017-09-04T15:19:12Z
date copyright	01/01/1952
date issued	1952
identifier other	MSONEEAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/18952
description abstract	An investigation was made of a 2:1 area ratio conical diffuser of length equal to the inlet diameter with separate variation of several basic parameters for simple nontwisted counterrotating rectangular vortex generators over a considerable range of inlet-boundary-layer thickness. The maximum values of static-pressure rise were determined for angle of attack, spacing, aspect ratio, and span-too-inlet boundary-layer thickness. Over the range of inlet-boundary-layer thickness it was shown that an increase in static-pressure rise of 40 percent could be obtained.
language	English
title	NACA-RM-L52B13	num
title	Effects of some primary variables of rectangular vortex generators on the static-pressure rise through a short diffuse	en
type	standard
page	33
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1952
contenttype	fulltext