NACA-TR-586

Airfoil section characteristics as affected by variations of the Reynolds numbe

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T16:32:56Z
date available	2017-09-04T16:32:56Z
date copyright	01/01/1937
date issued	1937
identifier other	USWUYDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/96377
description abstract	Report presents the results of an investigation of a systematically chosen representative group of related airfoils conducted in the NACA variable-density wind tunnel over a wide range of Reynolds number extending well into the flight range. The tests were made to provide information from which the variations of airfoil section characteristics with changes in the Reynolds number could be inferred and methods of allowing for these variations in practice could be determined. This work is one phase of an extensive and general airfoil investigation being conducted in the variable-density tunnel and extends the previously published researches concerning airfoil characteristics as affected by variations in airfoil profile determined at a single value of the Reynolds number.
language	English
title	NACA-TR-586	num
title	Airfoil section characteristics as affected by variations of the Reynolds numbe	en
type	standard
page	48
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1937
contenttype	fulltext