首页|Goal Programming for Stable Mode Transition in Tandem Turbo-ramjet Engines

Goal Programming for Stable Mode Transition in Tandem Turbo-ramjet Engines

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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.

propulsiontransitiongoal programming algorithmturbine-based combine cycle engineturbofan engineramjet enginehypersonic

Chen Min、Tang Hailong、Zhu Zhili

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School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

National Defense Basic Research Project

2009

中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDCSCDSCIEI
影响因子:0.847
ISSN:1000-9361
年,卷(期):2009.22(5)
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