Thermodinamically Compatible Conservation Laws for Working Process Simulation in High Temperature Air Breathing Engines and for Simulation of Some Nature Processes
The paper presents unified mathematical models of thermo-gas-dynamic process simulation for applied problems of air breathing engine creation and for theoretical analysis of some physics experimental data. In the first part of the paper we consider a coordination of thermodynamics and conservation laws by prediction of turbojet engine working process. This simulation is relevant to high class models based on real 3D geometry of turbojet engine flow path. They can be applied either in isolated unit components or in entire engine flow passage. The method of working process modeling considers all main features of engine working process (viscous and radiation losses, fuel application and combustion, air bleed and blow out, leakage from flow path, rotor and stator thermal dilatation, air humidity, rotor inertia and so on). The second part of the paper demonstrates simulation for explanation of new experimental data of modern physics. Here there are considered a few phenomenon and process which take place on a different scales (from atomic and nanotechnology scales up to astrophysical scales). We demonstrate simulations for astrophysics gamma-ray bursts, cosmic jets and dark matter.
M.Ja. Ivanov
Central Institude of Aviation Motors,Moscow,Russia
国际会议
4th International Symposium on Jet Propulsion and Power Engineering(第四届喷气推进与动力工程国际会议 ISJPPE2012)
西安
英文
3-12
2012-09-10（万方平台首次上网日期，不代表论文的发表时间）