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Goal Programming for Stable Mode Transition in Tandem Turbo-ramjet Engines 被引量:16
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作者 Chen Min Tang Hailong Zhu Zhili 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2009年第5期486-492,共7页
This article, in order to guarantee the stable mode transition in tandem turbo-ramjet engines, investigates the multi-objective and multi-variable goal programming algorithm. First, it introduces the structural featur... This article, in order to guarantee the stable mode transition in tandem turbo-ramjet engines, investigates the multi-objective and multi-variable goal programming algorithm. First, it introduces the structural features of the variable cycle turbo-ramjet engines, the principles of selecting the mode transition operation point and the design parameters, and the characteristics of the turbofan mode and the ramjet mode. Second, a component-based variable cycle turbo-ramjet engine model is developed to simulate the mode transition process. Third, the Newton-Raphson algorithm is used to solve the multi-variable and multi-objective optimization problem. The results show that with the maximum residua of only 0.06%, this algorithm has an acceptable convergence that meets the predetermined goals. Finally, the simulation shows that the stable turbo-ramjet mode transition could be realized with the mode transition control law developed by the algorithm. 展开更多
关键词 PROPULSION transition goal programming algorithm turbine-based combine cycle engine turbofan engine ramjetengine HYPERSONIC
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