Numerical Simulation of Internal Flow Field in Transonic Axial Compressor
Tao Ye, Fei Chen
Available Online April 2016.
- https://doi.org/10.2991/icmit-16.2016.66How to use a DOI?
- axial compressor; internal flow field; profile loss; numerical simulation; fitting
- The transonic axial compressor Stage35 was selected as a research object, using software NUMECA taking numerical simulation of it. And then, the distribution rules of pressure and temperature of meridional channel and blade surface are derived. On this basis, the formation process of shock wave and the influence of it on boundary layer were analyzed in detail. Using the least square cubic fit method, the characteristic curve of the compressor was fitted. The analysis results indicate that the profile loss makes the energy loss of compressor remarkable add, and the characteristic curve can be fitted precisely by using the least square cubic fit method.
- Open Access
- This is an open access article distributed under the CC BY-NC license.
Cite this article
TY - CONF AU - Tao Ye AU - Fei Chen PY - 2016/04 DA - 2016/04 TI - Numerical Simulation of Internal Flow Field in Transonic Axial Compressor BT - 2016 3rd International Conference on Mechatronics and Information Technology PB - Atlantis Press SN - 2352-538X UR - https://doi.org/10.2991/icmit-16.2016.66 DO - https://doi.org/10.2991/icmit-16.2016.66 ID - Ye2016/04 ER -