摘要
根据传热学和流体动力学理论,对燃气轮机空气系统流体动力学的计算方法进行了研究。得到了燃气轮机空气系统相关参数的计算模型。该方法易于理解,与模拟结果符合较好,计算精度满足实际工程分析需要。
Based on the theory of heat transfer and hydrokineties,the aerodynamics calculation methods about gas turbine secondary air system were studied. The calculation model on the relate parameters of gas turbine secondary air system has been obtained, showing that it is easy to understand, It＇ s result accord well with the simulation and the calculation accuracy meet the requirement of actual engineering analysis.
出处
《汽轮机技术》
北大核心
2010年第6期413-414,472,共3页
Turbine Technology
基金
国家863计划重型燃气轮机重大项目资助(项目编号:2008AA05A302)
关键词
燃气轮机
空气系统
gas turbine
secondary air system
