Investigation on the effects of the height of close canard wing on the aerodynamic characteristics of a forward-swept configuration

Jing Xia Zhan; Jin Jun Wang; Xia Zhao; Tian Li

Investigation on the effects of the height of close canard wing on the aerodynamic characteristics of a forward-swept configuration

Jing Xia Zhan^*
, Jin Jun Wang
, Xia Zhao
, Tian Li

^*此作品的通讯作者

航空科学与工程学院

Beihang University

科研成果: 期刊稿件 › 文章 › 同行评审

4 引用（Scopus）

摘要

Forward-swept configuration plays a more and more prominent role in the design of modern fighters because of its potential advantages. Force measurement in a low-speed wind tunnel was conducted to investigate the effects of the height of close canard wing on the longitudinal characteristics of a forward-swept configuration. The results indicate that it is more favorable for the aerodynamic characteristics to equip a higher close canard wing together with forward-swept angle of main wing increasing.

源语言	英语
页（从-至）	50-54
页数	5
期刊	Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics
卷	20
期	2
出版状态	已出版 - 6月 2006

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title = "Investigation on the effects of the height of close canard wing on the aerodynamic characteristics of a forward-swept configuration",

abstract = "Forward-swept configuration plays a more and more prominent role in the design of modern fighters because of its potential advantages. Force measurement in a low-speed wind tunnel was conducted to investigate the effects of the height of close canard wing on the longitudinal characteristics of a forward-swept configuration. The results indicate that it is more favorable for the aerodynamic characteristics to equip a higher close canard wing together with forward-swept angle of main wing increasing.",

keywords = "Close canard wing, Drag, Forward-swept wing, Lift, Lift-to-drag ratio",

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T1 - Investigation on the effects of the height of close canard wing on the aerodynamic characteristics of a forward-swept configuration

AU - Zhan, Jing Xia

AU - Wang, Jin Jun

AU - Zhao, Xia

AU - Li, Tian

PY - 2006/6

Y1 - 2006/6

N2 - Forward-swept configuration plays a more and more prominent role in the design of modern fighters because of its potential advantages. Force measurement in a low-speed wind tunnel was conducted to investigate the effects of the height of close canard wing on the longitudinal characteristics of a forward-swept configuration. The results indicate that it is more favorable for the aerodynamic characteristics to equip a higher close canard wing together with forward-swept angle of main wing increasing.

AB - Forward-swept configuration plays a more and more prominent role in the design of modern fighters because of its potential advantages. Force measurement in a low-speed wind tunnel was conducted to investigate the effects of the height of close canard wing on the longitudinal characteristics of a forward-swept configuration. The results indicate that it is more favorable for the aerodynamic characteristics to equip a higher close canard wing together with forward-swept angle of main wing increasing.

KW - Close canard wing

KW - Drag

KW - Forward-swept wing

KW - Lift

KW - Lift-to-drag ratio

UR - https://www.scopus.com/pages/publications/33747861140

M3 - 文章

AN - SCOPUS:33747861140

SN - 1672-9897

VL - 20

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JO - Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics

JF - Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics

IS - 2

ER -

Investigation on the effects of the height of close canard wing on the aerodynamic characteristics of a forward-swept configuration

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