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(dòng)機(jī)整機(jī)并發(fā)仿真接口,根據(jù)求解穩(wěn)態(tài)非線(xiàn)性方程組的并發(fā)分布式模型,通過(guò)與接口生成的存根和框架聯(lián)合開(kāi)發(fā)分別建立航空發(fā)動(dòng)機(jī)分布式仿真系統(tǒng)的服務(wù)和客戶(hù)程序,利用mfc開(kāi)發(fā)了人機(jī)交互界面。