NACA-ACR-L5F27

Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 65(sub 1)-210 airfoil section

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:55:18Z
date available	2017-09-04T15:55:18Z
date copyright	01/01/1945
date issued	1945
identifier other	QUUYYDAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;query=autho47037D83FCDCAC4261598F1EFDEC9FCD/handle/yse/58694
description abstract	An investigation was made of three interchangeable sealed-gap 0.20-airfoil –chord plain ailerons of different contour on the NACA 65-210 airfoil section. The three aileron contours tested were the true airfoil contour, straight sides, and a beveled trailing edge. The effects of aileron contour on the section aerodynamic characteristics of the airfoil and aileron are presented herein.
language	English
title	NACA-ACR-L5F27	num
title	Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 65(sub 1)-210 airfoil section	en
type	standard
page	59
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1945
contenttype	fulltext