| 1. | A concurrent simulation interface for full engine is defined , and then server and client programs are developed through co - coding the skeleton and stub which come from compiling predefined idl file , according to resolving the nonlinear equations group of concurrent distributed model
定义了航空发动机整机并发仿真接口,根据求解稳态非线性方程组的并发分布式模型,通过与接口生成的存根和框架联合开发分别建立航空发动机分布式仿真系统的服务和客户程序,利用mfc开发了人机交互界面。 |
