连续爆轰发动机热力学性质的数值模拟

周蕊; 王健平

连续爆轰发动机热力学性质的数值模拟

周蕊,
王健平

北京大学工学院湍流与复杂系统国家重点实验室,北京 100871

基金项目: 航空科学基金项目(2008ZH71006); 国家自然科学基金(10872006)

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出版历程
- 收稿日期: 2011-01-14
- 修回日期: 2011-06-10
- 刊出日期: 2012-01-28

Numerical investigation of thermodynamic performance on continuous detonation engines

State Key Laboratory of Turbulence and Complex System, Department of Mechanics and Aerospace Engineering, College of Engineering, Peking University, Beijing 100871, China

摘要

摘要: 在二维圆柱腔中连续爆轰发动机数值模拟的基础上,对喷入流场中的粒子进行跟踪,得到经历不同燃烧过程的粒子轨迹图.分析影响粒子轨迹及其上物理参量变化的主要因素.数值模拟得到相应的示功图和示热图,计算连续爆轰发动机的机械功及热效率,将数值模拟结果与理想ZND(Zeldovich-Neumann-Doring)模型进行定性和定量的比较,所得数值模拟结果与理论结果符合得很好,验证了连续爆轰发动机的优势.
- 连续爆轰发动机 /
- 热力学性质 /
- 数值模拟 /
- 轨迹 /
- 示功图 /
- 示热图
Abstract: Based on the two-dimensional(2-D) numerical simulation of continuous detonation engine in an annular chamber,the paths of fluid particles starting at the injection plate were tracked,and their thermodynamic condition was plotted on a p-v and T-s diagram.The main factors that affect the paths and the fluctuation of physical parameters were discussed in detail.The thermodynamic cycle efficiency and net work output were obtained from the diagrams.The numerical thermodynamic cycle diagrams show very similar structure to the ideal ZND(Zeldovich-Neumann-Doring) model.The superior performance of CDE(continuous detonation engine) is further defined.
- CDE(continuous detonation engine) /
- thermodynamic performance /
- numerical simulation /
- trajectory /
- p-v diagram /
- T-s diagram

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参考文献(15)

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