NACA-ARR-L4J05

Wind-tunnel investigation of an NACA 23021 airfoil with a 0.32-airfoil-chord double slotted flap

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T16:14:21Z
date available	2017-09-04T16:14:21Z
date copyright	01/01/1944
date issued	1944
identifier other	STUYYDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/77571
description abstract	An investigation was made in the LML 7- by 10-foot wind tunnel of an NACA 23021 airfoil with a double slotted flap having a chord 32 percent of the airfoil chord (0.32c) to determine the aerodynamic section characteristics with the flaps deflected at various positions. The effects of moving the fore flap and rear flap as a unit and of deflecting or removing the lower lap of the slot were also determined.
language	English
title	NACA-ARR-L4J05	num
title	Wind-tunnel investigation of an NACA 23021 airfoil with a 0.32-airfoil-chord double slotted flap	en
type	standard
page	54
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1944
contenttype	fulltext