摘要
This paper considers problems of the mathematical simulation of gas turbine engines and power plants.A program complex is presented which is capable of automatizing solutions of many problems concerning the theromo-gas-dynamic calculation of the engine flow passage at the stages of design,development and service.A universal mathematical model is provided which real- izes all calculation for engines of different structure schemes (including test-bench) under different regimes.This program complex includes modules WHICGBH.It can solve problems of optimiza- tion,identification and diagnostics.Software is realized on the computer ES and PC(IBM PC). Kazan Aviation Institute K.Marx Str.10 Kazan 420111 Elousi,USSR
This paper considers problems of the mathematical simulation of gas turbine engines and power plants.A program complex is presented which is capable of automatizing solutions of many problems concerning the theromo-gas-dynamic calculation of the engine flow passage at the stages of design,development and service.A universal mathematical model is provided which real- izes all calculation for engines of different structure schemes (including test-bench) under different regimes.This program complex includes modules WHICGBH.It can solve problems of optimiza- tion,identification and diagnostics.Software is realized on the computer ES and PC(IBM PC). Kazan Aviation Institute K.Marx Str.10 Kazan 420111 Elousi,USSR
