Numerical simulation on aerodynamic heating process and research on the missile head structure

Bowei Liu; Yanli Ma; Yi Jiang; Weichen Wang; Yongyuan Li; Liwu Shao

doi:10.1109/FCST.2010.47

Numerical simulation on aerodynamic heating process and research on the missile head structure

Bowei Liu^*, Yanli Ma, Yi Jiang, Weichen Wang, Yongyuan Li, Liwu Shao

^*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 calculate the aerodynamic heating process of the missile head, the environmental temperature and pressure are obtained by the ballistic trajectory table and the flight Mach number are calculated. The method of fluidsolid coupled was used to compute the inner and outer field of the missile. The temperature of the missile surface and head was obtained. The result shows the fluid-solid coupled method is suitable for the aerodynamic heating calculation. The inflexion of the missile should be considered respectively at the subsonic and the supersonic flight in the design of the missile.

Original language	English
Title of host publication	Proceedings - 5th International Conference on Frontier of Computer Science and Technology, FCST 2010
Pages	184-186
Number of pages	3
DOIs	https://doi.org/10.1109/FCST.2010.47
Publication status	Published - 2010
Event	5th International Conference on Frontier of Computer Science and Technology, FCST 2010 - Changchun, China Duration: 18 Aug 2010 → 22 Aug 2010

Publication series

Name	Proceedings - 5th International Conference on Frontier of Computer Science and Technology, FCST 2010

Conference

Conference	5th International Conference on Frontier of Computer Science and Technology, FCST 2010
Country/Territory	China
City	Changchun
Period	18/08/10 → 22/08/10

Keywords

Aerodynamic heating
Ballistic trajectory
Fluid-solid coupled
Numerical simulation
Shock wave

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10.1109/FCST.2010.47

Cite this

Liu, B., Ma, Y., Jiang, Y., Wang, W., Li, Y., & Shao, L. (2010). Numerical simulation on aerodynamic heating process and research on the missile head structure. In Proceedings - 5th International Conference on Frontier of Computer Science and Technology, FCST 2010 (pp. 184-186). Article 5575513 (Proceedings - 5th International Conference on Frontier of Computer Science and Technology, FCST 2010). https://doi.org/10.1109/FCST.2010.47

@inproceedings{1ee1cd3392614ac38394925487aa6292,

title = "Numerical simulation on aerodynamic heating process and research on the missile head structure",

abstract = "In order to calculate the aerodynamic heating process of the missile head, the environmental temperature and pressure are obtained by the ballistic trajectory table and the flight Mach number are calculated. The method of fluidsolid coupled was used to compute the inner and outer field of the missile. The temperature of the missile surface and head was obtained. The result shows the fluid-solid coupled method is suitable for the aerodynamic heating calculation. The inflexion of the missile should be considered respectively at the subsonic and the supersonic flight in the design of the missile.",

keywords = "Aerodynamic heating, Ballistic trajectory, Fluid-solid coupled, Numerical simulation, Shock wave",

author = "Bowei Liu and Yanli Ma and Yi Jiang and Weichen Wang and Yongyuan Li and Liwu Shao",

year = "2010",

doi = "10.1109/FCST.2010.47",

language = "English",

isbn = "9780769541396",

series = "Proceedings - 5th International Conference on Frontier of Computer Science and Technology, FCST 2010",

pages = "184--186",

booktitle = "Proceedings - 5th International Conference on Frontier of Computer Science and Technology, FCST 2010",

note = "5th International Conference on Frontier of Computer Science and Technology, FCST 2010 ; Conference date: 18-08-2010 Through 22-08-2010",

}

Liu, B, Ma, Y, Jiang, Y, Wang, W, Li, Y & Shao, L 2010, Numerical simulation on aerodynamic heating process and research on the missile head structure. in Proceedings - 5th International Conference on Frontier of Computer Science and Technology, FCST 2010., 5575513, Proceedings - 5th International Conference on Frontier of Computer Science and Technology, FCST 2010, pp. 184-186, 5th International Conference on Frontier of Computer Science and Technology, FCST 2010, Changchun, China, 18/08/10. https://doi.org/10.1109/FCST.2010.47

Numerical simulation on aerodynamic heating process and research on the missile head structure. / Liu, Bowei; Ma, Yanli; Jiang, Yi et al.
Proceedings - 5th International Conference on Frontier of Computer Science and Technology, FCST 2010. 2010. p. 184-186 5575513 (Proceedings - 5th International Conference on Frontier of Computer Science and Technology, FCST 2010).

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

TY - GEN

T1 - Numerical simulation on aerodynamic heating process and research on the missile head structure

AU - Liu, Bowei

AU - Ma, Yanli

AU - Jiang, Yi

AU - Wang, Weichen

AU - Li, Yongyuan

AU - Shao, Liwu

PY - 2010

Y1 - 2010

N2 - In order to calculate the aerodynamic heating process of the missile head, the environmental temperature and pressure are obtained by the ballistic trajectory table and the flight Mach number are calculated. The method of fluidsolid coupled was used to compute the inner and outer field of the missile. The temperature of the missile surface and head was obtained. The result shows the fluid-solid coupled method is suitable for the aerodynamic heating calculation. The inflexion of the missile should be considered respectively at the subsonic and the supersonic flight in the design of the missile.

AB - In order to calculate the aerodynamic heating process of the missile head, the environmental temperature and pressure are obtained by the ballistic trajectory table and the flight Mach number are calculated. The method of fluidsolid coupled was used to compute the inner and outer field of the missile. The temperature of the missile surface and head was obtained. The result shows the fluid-solid coupled method is suitable for the aerodynamic heating calculation. The inflexion of the missile should be considered respectively at the subsonic and the supersonic flight in the design of the missile.

KW - Aerodynamic heating

KW - Ballistic trajectory

KW - Fluid-solid coupled

KW - Numerical simulation

KW - Shock wave

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U2 - 10.1109/FCST.2010.47

DO - 10.1109/FCST.2010.47

M3 - Conference contribution

AN - SCOPUS:77957927635

SN - 9780769541396

T3 - Proceedings - 5th International Conference on Frontier of Computer Science and Technology, FCST 2010

SP - 184

EP - 186

BT - Proceedings - 5th International Conference on Frontier of Computer Science and Technology, FCST 2010

T2 - 5th International Conference on Frontier of Computer Science and Technology, FCST 2010

Y2 - 18 August 2010 through 22 August 2010

ER -

Liu B, Ma Y, Jiang Y, Wang W, Li Y, Shao L. Numerical simulation on aerodynamic heating process and research on the missile head structure. In Proceedings - 5th International Conference on Frontier of Computer Science and Technology, FCST 2010. 2010. p. 184-186. 5575513. (Proceedings - 5th International Conference on Frontier of Computer Science and Technology, FCST 2010). doi: 10.1109/FCST.2010.47

Numerical simulation on aerodynamic heating process and research on the missile head structure

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