贫氧燃烧

Oxygen-poor combustion

以上为机器翻译结果，快速获取精准的人工翻译结果，建议选择有道人工翻译

1
贫氧推进剂一次燃烧的物理和化学动力学因素决定了其一次燃烧为非平衡燃烧。
The primary combustion of deficient oxygen solid propellant is non equilibrium because of its own physical and chemical processes.
2
系统研究了铝镁贫氧推进剂低压燃烧特性的表征方法。
The characterization of the combustion properties of the aluminum? Magnesium fuel? Rich propellant for unchoked ducted rocket was studied.
3
说明了非平衡燃烧的特点，提出了计算贫氧推进剂一次燃烧的理论模型。
The features of non equilibrium combustion are shown, and the theoretical model is proposed.

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