|Table of Contents|

Numerical Simulation of Multiple Launch Rocket Whole Transient Heat Characteristics

《南京理工大学学报》（自然科学版）[ISSN:1005-9830/CN:32-1397/N]

Issue:
2010年01期
Page:
66-70
Research Field:
Publishing date:

Info

Title:
Numerical Simulation of Multiple Launch Rocket Whole Transient Heat Characteristics
Author(s):
ZHAO Ji-yong1; 2; MA Da-wei1; LE Gui-gao1
1.School of Mechanical Engineering,NUST,Nanjing 210094,China;2.Electronic and Electric Department,Changzhou Institute of Light Industry,Changzhou 213164,China
Keywords:
multiple launch rockets;  transient heat transfer;  decoupling;  heat analysis;  numerical simulation
PACS:
TJ393
DOI:
-
Abstract:
To realize the decoupling calculation of the internal and external coupling thermal effect of the multiple launch rocket control cabinet,the coupling heat transfer mechanism of the internal and external thermal environment of the multiple launch rocket control cabinet is analyzed,and an engineering calculation method of solving the internal and external coupling thermal effect of the multiple launch rocket control cabinet is established.The external heating effect of the combustion gas flow of the control cabinet is transformed into floating thermal boundary condition of the internal thermal analysis of the control cabinet when the multiple rocket launches continuously,avoiding a direct coupling solution.The transient heat condition in continuous launching is numerically simulated utilizing the above method and the internal transient temperature field of the control cabinet is obtained.The effects of some related factors are analyzed.It provides an important basis for designing finalization and relative research of multiple launch rockets.

References:

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Last Update: 2012-11-02