通过优化流通道结构,提高燃烧室水冷性能
Daijian Wu1,2, Guozheng Quan1, Fanxin Meng1
1Chongqing Key Laboratory of Advanced Mold Intelligent Manufacturing, School of Material Science and Engineering, Chongqing University, Chongqing 400044, China.
Materials (Basel, Switzerland)
|January 10, 2026
概括
优化拉姆喷气燃烧室设计至关重要. 一个有限元 (FE) 模型显示,0.3°的冷却通道斜率有效降低了内部压力,并优化了热流体结构相互作用.
科学领域:
- 航空航天工程 航空航天工程
- 热力学是一种热力学.
- 计算流体动力学的流体动力学.
背景情况:
- 高热风洞的进步需要改进喷气燃烧室设计.
- 复杂的操作环境对热和结构完整性构成重大挑战.
研究的目的:
- 开发和使用结合有限元 (FE) 模型来模拟雷姆喷气燃烧室的性能.
- 调查结构修改对流体流动,热行为和应力分布的影响.
主要方法:
- 使用计算流体动力学 (CFD) 进行数值模拟.
- 开发了一个热流体结构合FE模型.
- 在不同的结构参数下分析了燃烧室的使用条件.
主要成果:
- 在冷却水冲击墙壁时确定了双向流形成.
- 证明修改冷却水通道斜率有效降低燃烧室压力.
- 观察到输入应力降低,而输出应力随着通道斜率的改变而增加.
结论:
- 雷射燃烧室的最佳冷却水通道斜率被确定为0.3°.
- 这项研究为提高燃烧室设计和性能提供了关键的理论见解.
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