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 定義了航空發(fā)動機整機并發(fā)仿真接口,根據(jù)求解穩(wěn)態(tài)非線性方程組的并發(fā)分布式模型,通過與接口生成的存根和框架聯(lián)合開發(fā)分別建立航空發(fā)動機分布式仿真系統(tǒng)的服務和客戶程序,利用mfc開發(fā)了人機交互界面。