Regenerative Cooling for Liquid Rocket Engines
文献类型：期刊论文
| 作者 | Qi Feng |
| 刊名 | JOURNAL OF THERMAL SCIENCE
 |
| 出版日期 | 1995 |
| 卷号 | 4期号:1页码:54,58 |
| 关键词 | Liquid Propellant Rocket Engine Regenerative Cooling Thrust Chamber Heat Transfer| hydrogen|Transfer| hydrogen Methane Kerosene. |
| 英文摘要 | Heat transfer in the thrust chamber is of great importance in the design of liquid propellant rocket engines. Regenerative cooling is an advanced method which can ensure not only the proper running but also higher performance of a rocket engine. The theoretical model is complicated, it relates to fluid dynamics, heat transfer, combustion, etc... In this paper, a regenerative cooling model is presented. Effects such as radiation, heat transfer to environment, variable thermal properties and coking are included in the model. This model can be applied to all kinds of liquid propellant rocket engines as well as similar constructions. The modularized computer code is completed in the work. |
| 公开日期 | 2013-03-13 |
| 源URL | [http://ir.etp.ac.cn/handle/311046/54212]  |
| 专题 | 工程热物理研究所_Journal of Thermal Science |
| 推荐引用方式 GB/T 7714 | Qi Feng. Regenerative Cooling for Liquid Rocket Engines[J]. JOURNAL OF THERMAL SCIENCE,1995,4(1):54,58. |
| APA | Qi Feng.(1995).Regenerative Cooling for Liquid Rocket Engines.JOURNAL OF THERMAL SCIENCE,4(1),54,58. |
| MLA | Qi Feng."Regenerative Cooling for Liquid Rocket Engines".JOURNAL OF THERMAL SCIENCE 4.1(1995):54,58. |
入库方式： OAI收割
来源：工程热物理研究所
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