the results show, in the same entrance condition , the operating mode of scramjet combustor is influenced by the control of fuel .
计算研究表明,在相同的来流条件下,供油规律对燃烧室的工作模态有着重大的影响;
scramjet combustor may realize the subsonic-combustion mode and supersonic-combustion mode respectively based on the control of fuel in variable flight conditions.
在不同的来流条件下,可以通过调节供油规律使燃烧室分别实现亚燃模态和超燃模态;
scramjet combustor design optimization for a test scramjet model engine is conducted by employing genetic algorithms, and an optimal design much better than original design is obtained.
采用遗传算法对某试验超燃沖压模型发动机的燃烧室构型参数进行了优化设计,所得方案的性能大大优于实际方案。
the model of combustion efficiency for scramjet combustor is analyzed and presented in this paper.
本文分析及提出了超音速燃烧沖压发动机燃烧室燃烧效率的数学模型。
the methodology for scramjet combustor performance analysis and evaluation is build up.
提出了超燃沖压发动机燃烧室的性能分析评价方法。