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Aerodynamic improvement of a delta wing in combination with leading edge flaps
Aerodynamic improvement of a delta wing in combination with leading edge flaps
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摘要
未填写
DOI
lj1kyrv2dv/1820244
作者
Tadateru Ishide;Mao Itazawa
机构地区
不详
出处
《力学快报:英文版》
2017年6期
关键词
空气动力学
三角洲
翅膀
前缘
区域研究
粒子图象
分类
[理学][力学]
出版日期
2017年06月16日(中国期刊网平台首次上网日期,不代表论文的发表时间)
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William Ruffles;Sam M. Dakka.
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2
王晋军;张旺.
Experimental Investigations on Leading-Edge Vortex Structures for Flow over Non-Slender Delta Wings
.物理,2008-07.
3
Yan Zhang.
Effects of distributed leading-edge roughness on aerodynamic performance of a low-Reynolds-number airfoil: an experimental study
.力学,2018-03.
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MOHAMED Kaka LV Zhi-yong.
Longitudinal Aerodynamic Characteristics of the Novel Wing-Body
.计算机应用技术,2007-02.
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LARGE AERODYNAMIC FORCES ON A SWEEPING WING AT LOW REYNOLDS NUMBER
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Cheolheui Han.
Investigation of Unsteady Aerodynamic Characteristics of a Seagull Wing in Level Flight
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Azhar Muhammad;Quoc Viet Nguyen;Hoon Cheol Park;Do Y.Hwang;Doyoung Byun;Nam Seo Goo.
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.生物工程,2010-02.
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AUNG Ko Wynn CAO Yi-hua.
Analysis on Aerodynamic Performance of Finite Swept Wing with Glaze Ice Accretions
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.
Maintenance and Improvement of Delta-wave Current Power Supply
.物理,1997-10.
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Guoyu Luo Mao Sun.
The effects of corrugation and wing planform on the aerodynamic force production of sweeping model insect wings
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来源期刊
力学快报:英文版
2017年6期
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相关关键词
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前缘
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