NASA-TN-D-4448

Large-scale wind-tunnel tests of a deflected slipstream STOL model with wings of various aspect ratios

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T17:39:33Z
date available	2017-09-04T17:39:33Z
date copyright	01/01/1968
date issued	1968
identifier other	DSYKAEAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std/handle/yse/162552
description abstract	Wind tunnel determination of longitudinal force characteristics for STOL aircraft scale models with varying wing aspect ratios
language	English
title	NASA-TN-D-4448	num
title	Large-scale wind-tunnel tests of a deflected slipstream STOL model with wings of various aspect ratios	en
type	standard
page	56
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1968
contenttype	fulltext
subject keywords	AERODYNAMIC
subject keywords	AIRCRAFT
subject keywords	CHARACTERISTICS
subject keywords	CONTROL
subject keywords	EDGE
subject keywords	FLAPS
subject keywords	LIFT
subject keywords	LONGITUDINAL
subject keywords	MODELS
subject keywords	PROPELLER
subject keywords	SHORT
subject keywords	SLIPSTREAMS
subject keywords	STABILITY
subject keywords	TAKEOFF
subject keywords	TRAILING
subject keywords	TUNNEL
subject keywords	WIND