NACA-WR-L-454

Wind-tunnel investigation of control-surface characteristics VI - a 30-percent-chord plain flap on the NACA 0015 airfoil

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T17:03:06Z
date available	2017-09-04T17:03:06Z
date copyright	01/01/1942
date issued	1942
identifier other	BXXYYDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/126691
description abstract	Force-test measurements in two-dimensional flow have been made in the NACA 4- by 6-foot vertical tunnel of the characteristics of an NACA 0015 airfoil equipped with a plain flap having a chord 30 percent of the airfoil chord and a plain tab having a chord 20 percent of the flap chord. The results are presented in the form of aerodynamic section characteristics for several flap and tab deflections and for a sealed and an unsealed gap at the flap nose.
language	English
title	NACA-WR-L-454	num
title	Wind-tunnel investigation of control-surface characteristics VI - a 30-percent-chord plain flap on the NACA 0015 airfoil	en
type	standard
page	24
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1942
contenttype	fulltext