Application of turbulent reacting flow analysis in gas turbine combustor development

被引：3

作者：

Mandai, S

Nishida, H

机构：

[1] Mitsubishi Heavy Ind Co Ltd, Takasago Res & Dev Ctr, Takasago, Hyogo, Japan

[2] Kyushu Inst Technol, Dept Mech Engn, Tobata Ku, Kitakyushu, Fukuoka 8048550, Japan

来源：

JSME INTERNATIONAL JOURNAL SERIES B-FLUIDS AND THERMAL ENGINEERING | 2004年 / 47卷 / 01期

关键词：

turbulent reacting flow; CFD; diffusion combustion; premixed combustion; gas turbine combustor;

D O I：

10.1299/jsmeb.47.108

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

Developing a low NOX gas turbine combustor usually requires many experiments on flow and combustion. Computational prediction technology in the field of combustion has progressed with advances in computer technology and turbulent combustion models. This report covers applications of CFD for the development of the gas turbine combustor and some discrepancies between CFD and test results as well as improved methods for resolving such discrepancies.

引用

页码：108 / 114

页数：7