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《Acta Aeronautica Et Astronautica Sinica》 2008-03
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Integrated Design Optimization of Turbofan Engines Cycle for Multi-role Fighters

Chen Yuchun,Wang Xiaofeng,Tu Qiuye,Zhang Hong,Cai Yuanhu(School of Power and Energy,Northwestern Polytechnical University,Xi'an 710072,China)  
For studying the method of cycle parameters design optimization of turbofan engine,an integrated optimization design model of multirole fighters and turbofan engines is presented,and the computer program based on the model is developed.The model includes a bivariate controlled turbofan engine performance computing model,installed performance computing model,fighter dynamic analysis model,weight composing analysis model,mission profile analysis model,constraint and mission analysis model,and optimization computing model,etc.The study emphasis is to find the way of getting the constraint limitations of multi-role fighters.The multi-island genetic algorithm and adaptive simulated annealing are used to implement the cycle parameters design optimization for multi-role fighters in service,supercruising multi-role fighters without after-burning,and next generation advanced multi-role fighters.Some valuable conclusions for cycle parameters choice of turbofan engine are gained by analyzing the computation results.
【Fund】: 国家“863”计划项目(2006AA705403)
【CateGory Index】: V271.41
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