摘要
根据高马赫数流场特征参数变化快、固态场特征参数变化慢的特性,编制开发了针对高速气流的"半解耦"显式流固耦合近似计算程序,并通过数值方法分析了该方法的计算误差,分析结果显示其能够较准确地模拟高速流场与固态场长时间非稳态耦合问题。在此基础上,运用"半解耦"流固耦合方法数值模拟了高速气流横掠缝隙-腔体典型密封结构的非稳态过程,并与相关实验测试数据进行了对比,验证了程序可靠性。随后,进一步分析了气流侵入密封结构的主要特性,总结了密封结构内、外流场中气流温度、压力和速度的分布特征以及其随时间的变化规律,研究了密封结构中加热板气动热流随时间的变化规律,探讨了密封结构中固体温度场分布特征及其随时间积累的变化规律等。最终,计算结果说明了密封体的结构布局对其内部热状况的决定性影响。
In view of the fact that the characteristic parameters of a high Mach flow field vary much faster than those of the solid field,a program of approximate numerical simulation of the semi-decomposd fluid and solid coupling is developed and compiled.The calculating error of the method is analyzed by numerical simulation,and the results show that this method can accurately simulate the fluid and solid coupling in a high speed airflow field during a long unsteady process.The process of a high speed airflow impacting the seal structure is simulated by this method and the program is proved to be feasible after a comparison of the calculated results with the related experimental test.And then the features of the airflow invading the seal structure are analyzed.The contours of the flow field temperature,pressure and velocity inside and outside the seal structure and the their variation during the course of an unsteady process are summarized.The variation of the aerodynamic heat flux of the heating board with time is analyzed.The rules of the temperature variation of the seal structure with time are investigated.Finally,the results show that the structural layout of the seal plays a decisive role in the seal structure's thermal conditions.
出处
《航空学报》
EI
CAS
CSCD
北大核心
2012年第1期34-43,共10页
Acta Aeronautica et Astronautica Sinica
基金
国家自然科学基金(90816022)~~
关键词
流固耦合
高速气流
数值模拟
密封结构
非稳态过程
fluid and solid coupling
high speed airflow
numerical simulation
seal structure
unsteady process