NACA-WR-L-366

Wind-tunnel investigation of control-surface characteristics X - a 30-percent-chord plain flap with straight contour on the NACA 0015 airfoil

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T17:41:54Z
date available	2017-09-04T17:41:54Z
date copyright	01/01/1942
date issued	1942
identifier other	DZDZYDAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std/handle/yse/164915
description abstract	Force-test measurements in the-dimensional flow have been made in the NACA 4- by 6-foot vertical tunnel to determine the characteristics of an NACA 0015 airfoil equipped with a straight-contour plain flap having a chord 30 percent of the airfoil chord. The straight-contour plain flap differs from an ordinary plain flap in that the surfaces behind the hinge axis are flat instead of conforming to the - basic airfoil contour. The results are presented in the form of aerodynamic section characteristics for several flap deflections and for a sealed and unsealed gap at the flap dose.
language	English
title	NACA-WR-L-366	num
title	Wind-tunnel investigation of control-surface characteristics X - a 30-percent-chord plain flap with straight contour on the NACA 0015 airfoil	en
type	standard
page	17
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1942
contenttype	fulltext