NACA-TN-1422

Experimental and calculated characteristics of three wings of NACA 64-210 and 65-210 airfoil sections with and without 2 degree washout

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T16:09:29Z
date available	2017-09-04T16:09:29Z
date copyright	01/01/1947
date issued	1947
identifier other	SGTSYDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/72663
description abstract	Report presents the results of an investigation conducted to determine some of the effects of airfoil section and washout on the experimental and calculated characteristics of 10-percent-thick wings. Three wings of aspect ratio 9 and ratio of root chord to tip chord 2.5 were tested. One wing had NACA 64-210 sections and 2 degree washout, the second had NACA 65-210 sections and 2 degree washout, and the third had NACA 65-210 sections and 0 degree washout. It was found that the experimental characteristics of the wings could be satisfactorily predicted from calculations based upon two-dimensional data when the airfoil contours of the wings conformed to the true airfoil sections with the same high degree of accuracy as the two-dimensional models.
language	English
title	NACA-TN-1422	num
title	Experimental and calculated characteristics of three wings of NACA 64-210 and 65-210 airfoil sections with and without 2 degree washout	en
type	standard
page	18
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1947
contenttype	fulltext