NASA-TN-D-6826

Wind-tunnel investigation at low speeds of a model of the Kestrel (XV-6A) vectored-trust V/STOL airplane

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T16:16:34Z
date available	2017-09-04T16:16:34Z
date copyright	01/01/1972
date issued	1972
identifier other	BKYKAEAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/79913
description abstract	Longitudinal and lateral stability data were obtained with the model out of and in ground effect over a moving ground plane for a range of model angles of attack and sideslip at various thrust coefficients. These data were taken primarily at thrust coefficients which simulate transition speeds on the airplane between hover and 200 knots. Some data, however, represent the effect of thrust deflection at speeds up to 350 knots. Also presented are the effects of control-surface deflections and interference between the jets and free stream.
language	English
title	NASA-TN-D-6826	num
title	Wind-tunnel investigation at low speeds of a model of the Kestrel (XV-6A) vectored-trust V/STOL airplane	en
type	standard
page	179
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1972
contenttype	fulltext
subject keywords	AERODYNAMIC
subject keywords	AERODYNAMICS
subject keywords	AIRCRAFT
subject keywords	CHARACTERISTICS
subject keywords	CONFIGURATIONS
subject keywords	EFFECT
subject keywords	GROUND
subject keywords	MODELS
subject keywords	STABILITY
subject keywords	TESTS
subject keywords	TUNNEL
subject keywords	WIND