NACA-ACR-L4F23

Wind-tunnel investigation of control-surface characteristics XIX - a double flap with an overhang and an internal aerodynamic balance

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T17:03:53Z
date available	2017-09-04T17:03:53Z
date copyright	01/01/1944
date issued	1944
identifier other	XYDZYDAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;query=autho47037D83FCDCAC426159DD6E273C9FCD/handle/yse/127466
description abstract	Wind-tunnel tests have been made in two-dimensional flow to investigate the aerodynamic characteristics of a double flap with an internal and an overhang balance. Three sizes of each typee of balance were tested with three relative rates of deflection of the two flaps. An NAACA 66-009 airfoil having a 0.30-airfoil-chord straight-contour forward flap and.a 0.20-airfoil-chord straight-contour rearward flap was used.
language	English
title	NACA-ACR-L4F23	num
title	Wind-tunnel investigation of control-surface characteristics XIX - a double flap with an overhang and an internal aerodynamic balance	en
type	standard
page	53
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1944
contenttype	fulltext