These results can provide some reference for maintain and design for gas turbinecombustor.
本文研究结果可为发动机火焰筒的维修和改进设计提供参考。
2
The 3D numerical simulation of the QD128 aero-derivative gas turbinecombustor was performed by using computational fluid dynamics(CFD) software FLUENT.
应用计算流体动力学软件FLUENT，对QD128航改燃气轮机燃烧室进行了三维数值模拟计算分析。
3
A gas turbinecombustor includes a pilot burner, and a plurality of main burners disposed around the periphery of the pilot burner on the radially outer side.