Simplified procedure for controlling pressure distribution of a scramjet combustor |
| |
Authors: | Cui Tao |
| |
Institution: | School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China |
| |
Abstract: | Scramjet engines are used at extreme temperatures and velocity. New control problems involving distributed parameter control have been found concerning investigations of the control of scramjet engines whose physical states are spatially interacted. Succeeding the existing theoretical studies on the distributed parameter control for scramjet engines, this paper puts forward a simplified distributed parameter control approach for scramjet engines aimed at engineering application. The simplified control procedure uses the classical proportional-integral(PI) compensation to control the target pressure distribution of scramjet engines, which is effective and applicable for practical implements. Simulation results show the validation of the simplified distributed parameter control procedure. |
| |
Keywords: | Aeroengine Control Modeling Scramjet engine Supersonic combustion |
本文献已被 CNKI 维普 万方数据 ScienceDirect 等数据库收录! |