凝聚相微粒尺寸分布对固体火箭发动机燃烧室效率和喷管效率有影响。
The condensed phase particle size distribution affects the combustion chamber and nozzle efficiency of solid rocket motors to some extent.
针对微型燃气涡轮发动机喷嘴的雾化对燃烧室火焰稳定性、温度分布和燃烧效率的影响。
The nozzle spray characteristics of micro-turbine engines affect the stabilization of flame of the combustion chamber, the distribution of temperature, and the efficiency of combustion.
本文分析及提出了超音速燃烧冲压发动机燃烧室燃烧效率的数学模型。
The model of combustion efficiency for scramjet combustor is analyzed and presented in this paper.
燃烧室迷宫复合冷却结构是一种集冲击、对流换热和近似发散冷却于一身，结构合理，冷却效率高，具有创新性的新型冷却结构。
A combustors maze composite cooling structure is an innovative and highly efficient cooling structure that integrates impingement, convection heat exchange and approximate perspection cooling.
本文对装有钝体火焰稳定器的加力燃烧室燃烧效率特性进行了数值分析和实验研究。
This paper presents the combustion efficiency characteristics of an afterburner with bluff-body flame holders investigated with both numerical and experimental methods.
与你的燃烧室填补了冷却器、富氧空气、燃油燃烧在一个更有效率的混合物。
With your combustion chamber filled by cooler, oxygen-rich air, fuel burns at a more efficient mixture.
与你的燃烧室填补了冷却器、富氧空气、燃油燃烧在一个更有效率的混合物。
With your combustion chamber filled by cooler, oxygen-rich air, fuel burns at a more efficient mixture.
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