Notice of Retraction: Optimization design of the rocket launching facilities and the thermal protection

Yi Jiang; Yan Li Ma; Wei Chen Wang; Ji Guang Hao

doi:10.1109/ICACC.2010.5487017

Notice of Retraction: Optimization design of the rocket launching facilities and the thermal protection

Yi Jiang^*, Yan Li Ma, Wei Chen Wang, Ji Guang Hao

^*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 › 章节 › 同行评审

摘要

Based on fully hexahedral mesh and the k-e turbulence model, the computational fluid dynamics method was used to the numerical simulation. Different angle of the double-faced deflector and the thermal protection of the launching facilities were calculated. The pressure and temperature parameters were obtained and the result was compared and analyzed. The appropriate model was selected. The numerical calculation method and the results can be used to the engineering.

源语言	英语
主期刊名	Proceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010
出版商	IEEE Computer Society
页	30-33
页数	4
ISBN（印刷版）	9781424458462
DOI	https://doi.org/10.1109/ICACC.2010.5487017
出版状态	已出版 - 2010

出版系列

姓名	Proceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010
卷	5

访问文件

10.1109/ICACC.2010.5487017

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Jiang, Y., Ma, Y. L., Wang, W. C., & Hao, J. G. (2010). Notice of Retraction: Optimization design of the rocket launching facilities and the thermal protection. 在 Proceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010 (页码 30-33). 文章 5487017 (Proceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010; 卷 5). IEEE Computer Society. https://doi.org/10.1109/ICACC.2010.5487017

Jiang, Yi ; Ma, Yan Li ; Wang, Wei Chen 等. / Notice of Retraction : Optimization design of the rocket launching facilities and the thermal protection. Proceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010. IEEE Computer Society, 2010. 页码 30-33 (Proceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010).

@inbook{c5ad9865cd3d4c33b92ead14d0a37c6f,

title = "Notice of Retraction: Optimization design of the rocket launching facilities and the thermal protection",

abstract = "Based on fully hexahedral mesh and the k-e turbulence model, the computational fluid dynamics method was used to the numerical simulation. Different angle of the double-faced deflector and the thermal protection of the launching facilities were calculated. The pressure and temperature parameters were obtained and the result was compared and analyzed. The appropriate model was selected. The numerical calculation method and the results can be used to the engineering.",

keywords = "Deflector, Launching facilities, Rocket plume, Simulation, Thermal protection",

author = "Yi Jiang and Ma, {Yan Li} and Wang, {Wei Chen} and Hao, {Ji Guang}",

year = "2010",

doi = "10.1109/ICACC.2010.5487017",

language = "English",

isbn = "9781424458462",

series = "Proceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010",

publisher = "IEEE Computer Society",

pages = "30--33",

booktitle = "Proceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010",

address = "United States",

}

Jiang, Y, Ma, YL, Wang, WC & Hao, JG 2010, Notice of Retraction: Optimization design of the rocket launching facilities and the thermal protection. 在 Proceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010., 5487017, Proceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010, 卷 5, IEEE Computer Society, 页码 30-33. https://doi.org/10.1109/ICACC.2010.5487017

Notice of Retraction: Optimization design of the rocket launching facilities and the thermal protection. / Jiang, Yi; Ma, Yan Li; Wang, Wei Chen 等.
Proceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010. IEEE Computer Society, 2010. 页码 30-33 5487017 (Proceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010; 卷 5).

科研成果: 书/报告/会议事项章节 › 章节 › 同行评审

TY - CHAP

T1 - Notice of Retraction

T2 - Optimization design of the rocket launching facilities and the thermal protection

AU - Jiang, Yi

AU - Ma, Yan Li

AU - Wang, Wei Chen

AU - Hao, Ji Guang

PY - 2010

Y1 - 2010

N2 - Based on fully hexahedral mesh and the k-e turbulence model, the computational fluid dynamics method was used to the numerical simulation. Different angle of the double-faced deflector and the thermal protection of the launching facilities were calculated. The pressure and temperature parameters were obtained and the result was compared and analyzed. The appropriate model was selected. The numerical calculation method and the results can be used to the engineering.

AB - Based on fully hexahedral mesh and the k-e turbulence model, the computational fluid dynamics method was used to the numerical simulation. Different angle of the double-faced deflector and the thermal protection of the launching facilities were calculated. The pressure and temperature parameters were obtained and the result was compared and analyzed. The appropriate model was selected. The numerical calculation method and the results can be used to the engineering.

KW - Deflector

KW - Launching facilities

KW - Rocket plume

KW - Simulation

KW - Thermal protection

UR - http://www.scopus.com/inward/record.url?scp=77957936603&partnerID=8YFLogxK

U2 - 10.1109/ICACC.2010.5487017

DO - 10.1109/ICACC.2010.5487017

M3 - Chapter

AN - SCOPUS:77957936603

SN - 9781424458462

T3 - Proceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010

SP - 30

EP - 33

BT - Proceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010

PB - IEEE Computer Society

ER -

Jiang Y, Ma YL, Wang WC, Hao JG. Notice of Retraction: Optimization design of the rocket launching facilities and the thermal protection. 在 Proceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010. IEEE Computer Society. 2010. 页码 30-33. 5487017. (Proceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010). doi: 10.1109/ICACC.2010.5487017

Notice of Retraction: Optimization design of the rocket launching facilities and the thermal protection

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