Application of Gas-Kinetic BGK Scheme for Solving 2-D Compressible Inviscid Flow around Linear Turbine Cascade
Fluid flows within turbomachinery tend to be extremely complex. Understanding such flows is crucial in the effort to improve current turbomachinery designs. Hence, computational approaches can be used to great advantage in this regard. In this paper, gas-kinetic BGK (Bhatnagar-Gross-Krook) scheme is...
| Main Authors: | , , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Taylor & Francis
2006
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/5976/ http://irep.iium.edu.my/5976/ http://irep.iium.edu.my/5976/5/waqar_15502280600826357.fp.png_v03.pdf |