NASA-TN-D-363

Investigation of the aerodynamic characteristics of a combination jet-flap and deflected-slipstream configuration at zero and low forward speeds

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:27:34Z
date available	2017-09-04T15:27:34Z
date copyright	01/01/1960
date issued	1960
identifier other	NRTKAEAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/28508
description abstract	An investigation of the aerodynamic characteristics of a semispan wing equipped with a 38.5-percent-chord sliding flap partially immersed in the slipstream of two propellers has been conducted in the 17-foot test section of the Langeley 300-MPH 7- by 10-foot tunnel. The wing had an aspect ratio of 7.0, taper ratio 1.0, and an NACA 63A412 airfoil section. The propellers were one wing chord in diameter. A jet of air was ejected over the knee of the flap through a momentum-coefficient range from zero to about 1.0.
language	English
title	NASA-TN-D-363	num
title	Investigation of the aerodynamic characteristics of a combination jet-flap and deflected-slipstream configuration at zero and low forward speeds	en
type	standard
page	73
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1960
contenttype	fulltext
subject keywords	AERODYNAMIC
subject keywords	AIR
subject keywords	CHARACTERISTICS
subject keywords	COEFFICIENTS
subject keywords	CONTROL
subject keywords	DEFLECTION
subject keywords	DISTRIBUTION
subject keywords	FLAPS
subject keywords	FLOW
subject keywords	JET
subject keywords	PRESSURE
subject keywords	SURFACES
subject keywords	WING