Validation of turbine blade geometry by using a modified equation Spalart Allmaras turbulent model / Muhammad`Azim Samsuwar
The study represents the validation of one equation turbulence model (Spalart Allmaras) that incorporates fixed variables of exit Reynolds number is 2.8 x 10# and the exit isentropic Mach number is 0.79 on a turbine blade geometry. The computational simulation is done by ANSYS 16.2 with a minimum gr...
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| 格式: | Thesis |
| 語言: | English |
| 出版: |
2019
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| 在線閱讀: | https://ir.uitm.edu.my/id/eprint/89188/1/89188.pdf https://ir.uitm.edu.my/id/eprint/89188/ |
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