Abstract
An aviation gas turbine engine numerical simulation system is developed for simulation of steady and transient working processes in aviation gas turbine engine. This paper introduced the mathematical models of gas Thermodynamic process in the flow passage of aviation gas turbine engines. The modeling and engine performance analyzing were accomplished. This paper shows the performance simulation model of aviation gas turbine engine. This paper presents typical results for simulation of steady and transient processes for various types of ga s turbine engines. These results are compared very widely with experimental data, obtained for full-scale engines. Nomenclature
Sign-in/Register to access full text options 
Free) 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a call
