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

^*Corresponding author for this work

School of Aeronautic Science and Engineering

Beihang University

Research output: Contribution to journal › Article › peer-review

4 Scopus citations

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.

Original language	English
Pages (from-to)	50-54
Number of pages	5
Journal	Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics
Volume	20
Issue number	2
State	Published - Jun 2006

Keywords

Close canard wing
Drag
Forward-swept wing
Lift
Lift-to-drag ratio

Cite this

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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",

author = "Zhan, \{Jing Xia\} and Wang, \{Jin Jun\} and Xia Zhao and Tian Li",

year = "2006",

month = jun,

language = "英语",

volume = "20",

pages = "50--54",

journal = "Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics",

issn = "1672-9897",

publisher = "Zhongguo Kongqi Dongli Yanjiu yu Fazhan Zhongxin",

number = "2",

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TY - JOUR

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

SP - 50

EP - 54

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

Abstract

Keywords

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