CFD Simulation of Combustion in Gas Turbine Engine
Xingxia Hou, Shaolin Wang, Pengfu Xie, Qing Gao, Chunqing Tan, Jianwen Wang
Available Online April 2017.
- https://doi.org/10.2991/fmsmt-17.2017.170How to use a DOI?
- Numerical simulation, strong swirl combustor, turbulence model, combustion model.
- In order to investigate the liquid fuel combustion in gas turbine engine, the velocity of field and temperature of combustor in lean fuel injection model were numerically simulated and compared with the experimental data. The results show that the Realizable k- turbulence model can simulate the combustion in the strong swirl combustion chamber well, and numerical results of the non-premixed combustion model and the DO heat transfer model were in good agreement with experimental data. According to the contrast of velocity field, it can be found that the recir-culation zone expands in radial direction and contracts in axial direction for reacting case, which was compared with that of non-reacting case. This work laid the foundation for CFD simulation of gas turbine combustor and analysis of velocity profile.
- Open Access
- This is an open access article distributed under the CC BY-NC license.
Cite this article
TY - CONF AU - Xingxia Hou AU - Shaolin Wang AU - Pengfu Xie AU - Qing Gao AU - Chunqing Tan AU - Jianwen Wang PY - 2017/04 DA - 2017/04 TI - CFD Simulation of Combustion in Gas Turbine Engine BT - Proceedings of the 2017 5th International Conference on Frontiers of Manufacturing Science and Measuring Technology (FMSMT 2017) PB - Atlantis Press SP - 890 EP - 896 SN - 2352-5401 UR - https://doi.org/10.2991/fmsmt-17.2017.170 DO - https://doi.org/10.2991/fmsmt-17.2017.170 ID - Hou2017/04 ER -