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以超声速/高超声速飞机用预冷式涡喷发动机为研究对象,提出利用多目标遗传算法,根据用途、燃料和巡航马赫数的不同选定最佳发动机参数的方法,介绍了分析方法及其结果。
Taking the precooling turbojet engine for supersonic / hypersonic aircraft as the research object, this paper proposes a multi-objective genetic algorithm to select the optimal engine parameters according to the purpose, fuel and cruise Mach number. The analytical methods and their results .