Proceedings of the 2016 3rd International Conference on Mechatronics and Information Technology

Numerical Simulation of Internal Flow Field in Transonic Axial Compressor

Authors
Tao Ye, Fei Chen
Corresponding Author
Tao Ye
Available Online April 2016.
DOI
https://doi.org/10.2991/icmit-16.2016.66How to use a DOI?
Keywords
axial compressor; internal flow field; profile loss; numerical simulation; fitting
Abstract
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.
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Proceedings
2016 3rd International Conference on Mechatronics and Information Technology
Part of series
Advances in Computer Science Research
Publication Date
April 2016
ISBN
978-94-6252-184-1
ISSN
2352-538X
DOI
https://doi.org/10.2991/icmit-16.2016.66How to use a DOI?
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  -