The length scale effect between wall and closes field point on a single turbine blade simulation / Mohd Hafiz Mohd Noh ... [et al.]

A numerical code has been developed based on experiment data, by using Finite Volume Method. Four different turbulence models (one equation model) have been tested; Spalart-Allmaras, Delay Eddy Simulation, Delay Detached Eddy Simulation and Improve Delayed Detached Eddy Simulation. The exit Reynolds...

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Bibliographic Details
Main Authors: Mohd Noh, Mohd Hafiz (Author), Abdul Hamid, Ahmad Hussein (Author), Koichi, Mori (Author)
Format: Book
Published: Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM), 2018.
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100 1 0 |a Mohd Noh, Mohd Hafiz  |e author 
700 1 0 |a Abdul Hamid, Ahmad Hussein  |e author 
700 1 0 |a Koichi, Mori  |e author 
245 0 0 |a The length scale effect between wall and closes field point on a single turbine blade simulation / Mohd Hafiz Mohd Noh ... [et al.] 
260 |b Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM),   |c 2018. 
500 |a https://ir.uitm.edu.my/id/eprint/40964/1/40964.pdf 
520 |a A numerical code has been developed based on experiment data, by using Finite Volume Method. Four different turbulence models (one equation model) have been tested; Spalart-Allmaras, Delay Eddy Simulation, Delay Detached Eddy Simulation and Improve Delayed Detached Eddy Simulation. The exit Reynolds number is 2.8  106 and the exit isentropic Mach number is 0.79. The code has been validated with isentropic Mach number around the blade, trailing edge pressure distribution, vortex shedding frequency at S/D=-0.62 and boundary layer profile at a distance equal to one. DDES has shown a good agreement qualitatively and quantitatively with the experiment as compared with others and at region -1<S/D<1, all results show insignificant different. 
546 |a en 
690 |a Mechanics applied to machinery. Dynamics 
690 |a Hydraulic machinery 
655 7 |a Article  |2 local 
655 7 |a PeerReviewed  |2 local 
787 0 |n https://ir.uitm.edu.my/id/eprint/40964/ 
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