Numerical simulation for aerodynamic characteristics of low altitude and subsonic flight vehicle

Liwu Shao; Yanli Ma; Yi Jiang; Jiguang Hao; Bowei Liu

doi:10.1109/ISSCAA.2010.5633191

Numerical simulation for aerodynamic characteristics of low altitude and subsonic flight vehicle

Liwu Shao^*, Yanli Ma, Yi Jiang, Jiguang Hao, Bowei Liu

^*此作品的通讯作者

宇航学院

Beijing Institute of Technology

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

摘要

In order to analyze the drag characteristics of the vehicle having different war head and empennage, the computational fluid dynamics numerical simulation was used. The method was based on fully hexahedral mesh and three-dimensional Navier-Stokes equations and Spalart-Allmaras turbulence model. Through numerical simulation the flow field structures and computational aerodynamic characteristics were obtained. The results showed that using Kaman figure war head and proper trapeziform empennage can reduce the drag characteristics of the missile and the results will provide evidence to optimize the configuration of the missile in engineering design.

源语言	英语
主期刊名	ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics
页	578-581
页数	4
DOI	https://doi.org/10.1109/ISSCAA.2010.5633191
出版状态	已出版 - 2010
活动	3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010 - Harbin, 中国期限: 8 6月 2010 → 10 6月 2010

出版系列

姓名	ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics

会议

会议	3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010
国家/地区	中国
市	Harbin
时期	8/06/10 → 10/06/10

访问文件

10.1109/ISSCAA.2010.5633191

其它文件与链接

链接到 Scopus 的出版物

引用此

Shao, L., Ma, Y., Jiang, Y., Hao, J., & Liu, B. (2010). Numerical simulation for aerodynamic characteristics of low altitude and subsonic flight vehicle. 在 ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics (页码 578-581). 文章 5633191 (ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics). https://doi.org/10.1109/ISSCAA.2010.5633191

@inproceedings{5645972949ad4841a022914218680aef,

title = "Numerical simulation for aerodynamic characteristics of low altitude and subsonic flight vehicle",

abstract = "In order to analyze the drag characteristics of the vehicle having different war head and empennage, the computational fluid dynamics numerical simulation was used. The method was based on fully hexahedral mesh and three-dimensional Navier-Stokes equations and Spalart-Allmaras turbulence model. Through numerical simulation the flow field structures and computational aerodynamic characteristics were obtained. The results showed that using Kaman figure war head and proper trapeziform empennage can reduce the drag characteristics of the missile and the results will provide evidence to optimize the configuration of the missile in engineering design.",

keywords = "Drag characteristics, Numerical simulation, Stabilization, Trapeziform empennage, Wrap around empennage",

author = "Liwu Shao and Yanli Ma and Yi Jiang and Jiguang Hao and Bowei Liu",

year = "2010",

doi = "10.1109/ISSCAA.2010.5633191",

language = "English",

isbn = "9781424460441",

series = "ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics",

pages = "578--581",

booktitle = "ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics",

note = "3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010 ; Conference date: 08-06-2010 Through 10-06-2010",

}

Shao, L, Ma, Y, Jiang, Y, Hao, J & Liu, B 2010, Numerical simulation for aerodynamic characteristics of low altitude and subsonic flight vehicle. 在 ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics., 5633191, ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics, 页码 578-581, 3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010, Harbin, 中国, 8/06/10. https://doi.org/10.1109/ISSCAA.2010.5633191

Numerical simulation for aerodynamic characteristics of low altitude and subsonic flight vehicle. / Shao, Liwu; Ma, Yanli; Jiang, Yi 等.
ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics. 2010. 页码 578-581 5633191 (ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics).

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

TY - GEN

T1 - Numerical simulation for aerodynamic characteristics of low altitude and subsonic flight vehicle

AU - Shao, Liwu

AU - Ma, Yanli

AU - Jiang, Yi

AU - Hao, Jiguang

AU - Liu, Bowei

PY - 2010

Y1 - 2010

N2 - In order to analyze the drag characteristics of the vehicle having different war head and empennage, the computational fluid dynamics numerical simulation was used. The method was based on fully hexahedral mesh and three-dimensional Navier-Stokes equations and Spalart-Allmaras turbulence model. Through numerical simulation the flow field structures and computational aerodynamic characteristics were obtained. The results showed that using Kaman figure war head and proper trapeziform empennage can reduce the drag characteristics of the missile and the results will provide evidence to optimize the configuration of the missile in engineering design.

AB - In order to analyze the drag characteristics of the vehicle having different war head and empennage, the computational fluid dynamics numerical simulation was used. The method was based on fully hexahedral mesh and three-dimensional Navier-Stokes equations and Spalart-Allmaras turbulence model. Through numerical simulation the flow field structures and computational aerodynamic characteristics were obtained. The results showed that using Kaman figure war head and proper trapeziform empennage can reduce the drag characteristics of the missile and the results will provide evidence to optimize the configuration of the missile in engineering design.

KW - Drag characteristics

KW - Numerical simulation

KW - Stabilization

KW - Trapeziform empennage

KW - Wrap around empennage

UR - http://www.scopus.com/inward/record.url?scp=79952153364&partnerID=8YFLogxK

U2 - 10.1109/ISSCAA.2010.5633191

DO - 10.1109/ISSCAA.2010.5633191

M3 - Conference contribution

AN - SCOPUS:79952153364

SN - 9781424460441

T3 - ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics

SP - 578

EP - 581

BT - ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics

T2 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010

Y2 - 8 June 2010 through 10 June 2010

ER -

Shao L, Ma Y, Jiang Y, Hao J, Liu B. Numerical simulation for aerodynamic characteristics of low altitude and subsonic flight vehicle. 在 ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics. 2010. 页码 578-581. 5633191. (ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics). doi: 10.1109/ISSCAA.2010.5633191

Numerical simulation for aerodynamic characteristics of low altitude and subsonic flight vehicle

摘要

出版系列

会议

访问文件

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引用此