NACA-TR-628

Aerodynamic characteristics of a large number of airfoils tested in the variable-density wind tunnel

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:45:59Z
date available	2017-09-04T15:45:59Z
date copyright	01/01/1938
date issued	1938
identifier other	PTWUYDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/48628
description abstract	airfoils tested in the variable-density tunnel have been reduced to a comparable form and are published in this report for convenient reference. Plots of the standard characteristics are given in tabular form. Included is a tabulation of important characteristics for the related airfoils reported in NACA report 460. This report, in conjunction with NACA report 610, makes available in comparable and convenient form the aerodynamic data for airfoils tested in the variable-density tunnel since January 1, 1931.
language	English
title	NACA-TR-628	num
title	Aerodynamic characteristics of a large number of airfoils tested in the variable-density wind tunnel	en
type	standard
page	56
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1938
contenttype	fulltext