液膜再生复合冷却中液膜传热特性

杨薇; 孙冰

液膜再生复合冷却中液膜传热特性

杨薇,
孙冰

北京航空航天大学宇航学院,北京 100191

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- 被引次数: 0
出版历程
- 收稿日期: 2010-09-29
- 修回日期: 2010-12-31
- 刊出日期: 2011-09-28

Thermal characteristics of liquid film in a film regenerative cooling system

YANG Wei,
SUN Bing

School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

摘要

摘要: 对液体火箭发动机液膜再生复合冷却进行了算法研究.综合考虑了发动机内部化学反应、蒸发、卷吸、对流、导热、辐射等因素,将冷却液膜分为显热区、潜热区及气膜区三个区域进行了计算.推导了液膜长度和厚度的计算方法,分析了液膜再生复合冷却效率及各因素对液膜传热特性的影响.计算结果表明:①液膜入口质量流量越大,液膜区长度越长,冷却效率越高,复合冷却效率可维持在0.57以上.②高温燃烧室内膜的液体段长度很短,在液膜存在区域内冷却效率高达0.9.③液膜消失后,头部冷却液膜的设计仍对室壁起了很好的冷却保护作用,低温边区一直延伸至出口.④液膜吸收的显热和液膜蒸发吸收的热量及高温燃气与膜间的对流在液膜区内起了主要作用,而卷吸造成的质量损失及传热不可忽略.
- 液体火箭发动机 /
- 液膜再生复合冷却 /
- 冷却效率 /
- 传热 /
- 质量损失
Abstract: Computation method on film regenerative cooling in liquid rocket was studied in this paper.To integrate the factors such as chemistry,evaporation,entrainment,convection,thermal conductivity and radiation,the liquid film was divided into three areas-temperature increase area,evaporation area and steam area to be calculated.Length and thickness of the film were computed,and effects of these factors on film were analyzed.The results show that: (1) Length of liquid film and cooling effectiveness is obviously enhanced with the increase of the film coolant mass flow,and the associated cooling effectiveness is up to 0.57 .(2) Length of liquid film is short in hot combustor,but the cooling effectiveness is up to 0.9 in this area .(3) The film in the head of combustor protects the whole wall even if the liquid has disappeared.Low temperature border area covers the whole combustor .(4) Sensible heat absorbed by the liquid film,evaporation heat of the film and convection heat from hot gas to liquid film are most important elements in liquid film area.However,mass loss and heat transfer caused by entrainment should not be ignored.
- liquid rocket engine /
- film regenerative cooling /
- cooling effectiveness /
- heat transfer /
- mass loss

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