The Optimization of Combustion Chamber Components with Constrained Axisymmetric Sensitivity Analysis Algorithm

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Abstract:

To improve the situation of stress concentration in the combustion chamber component, optimized the design of combustion chamber shell structures is required. In this paper, a new boundary element integrated optimization method is used. There are a symmetry axis structure and effective constrained optimization model for sensitivity analysis. The technology and the general shape optimization algorithm are combined. The components' shape of the combustion chamber's shell under a plane stress is optimized, and finally, the satisfactory results are obtained and the maximum tangential bore stress is reduced.

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Periodical:

Advanced Materials Research (Volumes 287-290)

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73-76

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Online since:

July 2011

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© 2011 Trans Tech Publications Ltd. All Rights Reserved

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[1] Lianhua YIN, Li LIU,Optimization of the thermal structure of Flight Summary,Tactical Missile Technology,2006 (5): 53-58.

Google Scholar

[2] Dexin ZHANG, Shape optimization of all analytical sensitivity analysis(SCI Indexed), Applied Mathematics and Mechanics,2001.(22):1193-1200.

Google Scholar

[3] Dexin ZHANG, Constrained optimization with a Predicted effective method of design of the combustion chamber components. THERMAL ENERGY AND POWER 2008.23;60-63[7]

Google Scholar