Numerical Analysis of Active Cooling Structure of Engine Combustion Chamber

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Abstract:

With the convective heat transfer theory, numerical analysis of fluid-solid-heat coupling is implemented for the engine combustion chamber cooling structure based on finite element method and computational fluid dynamic method, thus to obtain valuable simulation results. Different components of the mesh generation method used which have different influences on the computational results are thought over during this analysis process, including different grid type, grid density and boundary layer meshes. Moreover, MPI parallel technique is also used to resolve the computation demands. The temperature distributions of the key parts in the cooling structure are investigated, which can be used as a significant reference for the thermal protection design of the engine combustion chamber.

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564-569

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December 2012

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© 2013 Trans Tech Publications Ltd. All Rights Reserved

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[1] Zhong FQ, Fan XJ, Gang YU.Heat transfer analysis for actively cooled supersoniccombustor. Journal of Propulsion Technology, 2009, 6: 1001-1012.

Google Scholar

[2] Wang QW, Wu F. The channel of liquid rocket engine thrust chamber. Numerical simulation and optimization on heat transfer and fluid flow in cooling ineering and Software, 2006, 23 : 907-921.

DOI: 10.1108/02644400610707793

Google Scholar

[3] Naraghi MH. A computer code for three dimensional rocket thermal evaluation,user manual for RTE2002 version.Tara Technologies,LLC,2002.

Google Scholar

[4] Niu L, Cheng HE. Analysis of heat transfer for regenerative cooling channel of platelet thrust chamber. Journal Of Propulsion Technology,2001.

Google Scholar

[5] Li JW, Liu Y. Method of Computing Temperature Field in Regeneratively-Cooled Thrust Chamber. Journal of Aerospace Power, 1000-8055,2004.

Google Scholar

[6] Jiang J. The research of scramjet combustion chamber regenerative cooling.Shan'xi: Doctoral thesis, Northwestern Polytechnical University.2006.

Google Scholar

[7] Al-Zaharanah IT, Yibas BS, Hashmi M SJ. Conjugate heat transfer in fully developed laminar pipe flow and thermally induced stresses. Computer Methods Applied Mechanic Engineering,2000,190:1091-1104.

DOI: 10.1016/s0045-7825(99)00467-3

Google Scholar

[8] Luna N, Mendez F, Trevino T. Conjugated heat transfer in circular ducts with a power-law laminar convection fluid flow. International Journal of Heat Mass Transfer,2002,45:655-666\"".

DOI: 10.1016/s0017-9310(01)00147-8

Google Scholar

[9] Bilir S. Transient conjugated heat transfer in pipes involving two-dimensional wall and axiak fluid conduction .International Journal of Heat Mass Transfer,2002,45:1781-1788.

DOI: 10.1016/s0017-9310(01)00270-8

Google Scholar

[10] Yapici H, Albayrak B. Numerical solutions of conjugate heat transfer and thermal stresses in a circular pipe externally heated with non-uniform heat flux. Energy Conversion and Management, 2004, 45: 927-937.

DOI: 10.1016/s0196-8904(03)00195-x

Google Scholar

[11] Kays WM, Crawford ME, Weigand B. Convective Heat and Mass Transfer. New York: McGraw-Hill, 2007.

Google Scholar

[12] Bai YG, Sun DK, Lin JH, et al. Numerical aerodynamic simulations of a NACA airfoil using CFD with block-iterative coupling and turbulence modelling. International Journal of Computational Fluid Dynamics, 2012, 26(2): 119-132.

DOI: 10.1080/10618562.2011.646997

Google Scholar