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

^*Corresponding author for this work

School of Aerospace Engineering

Beijing Institute of Technology

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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.

Original language	English
Title of host publication	ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics
Pages	578-581
Number of pages	4
DOIs	https://doi.org/10.1109/ISSCAA.2010.5633191
Publication status	Published - 2010
Event	3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010 - Harbin, China Duration: 8 Jun 2010 → 10 Jun 2010

Publication series

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

Conference

Conference	3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010
Country/Territory	China
City	Harbin
Period	8/06/10 → 10/06/10

Keywords

Drag characteristics
Numerical simulation
Stabilization
Trapeziform empennage
Wrap around empennage

Access to Document

10.1109/ISSCAA.2010.5633191

Cite this

Shao, L., Ma, Y., Jiang, Y., Hao, J., & Liu, B. (2010). Numerical simulation for aerodynamic characteristics of low altitude and subsonic flight vehicle. In ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics (pp. 578-581). Article 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. in 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, pp. 578-581, 3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010, Harbin, China, 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 et al.
ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics. 2010. p. 578-581 5633191 (ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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

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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. In ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics. 2010. p. 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

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