NACA-RM-L51A23

Flight determination of the effects of wing vortex generators of the aerodynamic characteristics of the Douglas D-558-I airplane

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T17:01:31Z
date available	2017-09-04T17:01:31Z
date copyright	01/01/1951
date issued	1951
identifier other	XRONEEAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/125010
description abstract	Tests were made of the Douglas D-558-1 airplane to determine the effect of wing vortex generators on some of the typical undesirable handling characteristics such as buffeting, lateral unsteadiness, change in trim, and loss in control effectiveness which have occurred on present-day aircraft flying at supercritical speeds. An arbitrary size, shape, and location of the generators were selected and the investigation was initiated to determine what benefits might be derived from the installation and whether further investigations would be warranted.
language	English
title	NACA-RM-L51A23	num
title	Flight determination of the effects of wing vortex generators of the aerodynamic characteristics of the Douglas D-558-I airplane	en
type	standard
page	24
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1951
contenttype	fulltext