The supersonic combustion chamber inlet is a 2 D convergent - divergent nozzle.
高超音速冲压发动机由进气道、超音速燃烧室和喷管组成.
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The mixture - fraction equilibrium chemistry model and discrete droplet model can predict correctly kerosene spray supersonic combustion.
混合分数平衡化学反应模型和离散液滴模型能准确地预测煤油在双模态燃烧室内的喷雾燃烧.
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