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Windsor Body 2.5 degree yaw unsteady CFD Simulation
This is a simulation of the Windsor body at 2.5 degree yaw in the Loughborough University wind tunnel. It is a test case in the Third Automotive CFD Prediction workshop. An isosurface of the Q criterion parameter is used to extract vortex cores and the video shows the unsteadiness in the wake. The f...
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| Format: | Data Audio/Video |
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2022
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| Online Access: | https://dx.doi.org/10.17028/rd.lboro.20089283.v1 |
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| _version_ | 1818165661123215360 |
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| author | Gary Page |
| author_facet | Gary Page |
| author_sort | Gary Page (1171617) |
| collection | Figshare |
| description | This is a simulation of the Windsor body at 2.5 degree yaw in the Loughborough University wind tunnel. It is a test case in the Third Automotive CFD Prediction workshop. An isosurface of the Q criterion parameter is used to extract vortex cores and the video shows the unsteadiness in the wake. The four green planes correspond to the location of the laser sheets used in the experiment to measure the velocity field. The second video animates the velocity field in the laser sheets in a similar manner to the experimental PIV measurements. The calculations were carried out using STAR-CCM+ 17.02 on the standard workshop grid g2 and with a Detached Eddy Simulation to capture the large scale turbulence. |
| format | Data Audio/Video |
| id | rr-article-20089283 |
| institution | Loughborough University |
| publishDate | 2022 |
| record_format | Figshare |
| spelling | rr-article-200892832022-11-30T13:23:12Z Windsor Body 2.5 degree yaw unsteady CFD Simulation Gary Page (1171617) Automotive engineering not elsewhere classified Aerodynamics (excl. hypersonic aerodynamics) CFD aerodynamics Automotive Engineering not elsewhere classified Aerodynamics (excl. Hypersonic Aerodynamics) Computational Fluid Dynamics <p>This is a simulation of the Windsor body at 2.5 degree yaw in the Loughborough University wind tunnel. It is a test case in the Third Automotive CFD Prediction workshop. An isosurface of the Q criterion parameter is used to extract vortex cores and the video shows the unsteadiness in the wake. The four green planes correspond to the location of the laser sheets used in the experiment to measure the velocity field. The second video animates the velocity field in the laser sheets in a similar manner to the experimental PIV measurements. The calculations were carried out using STAR-CCM+ 17.02 on the standard workshop grid g2 and with a Detached Eddy Simulation to capture the large scale turbulence.</p> 2022-11-30T13:23:12Z Dataset Media 10.17028/rd.lboro.20089283.v1 https://figshare.com/articles/media/Windsor_Body_2_5_degree_yaw_unsteady_CFD_Simulation/20089283 CC BY-NC 4.0 |
| spellingShingle | Automotive engineering not elsewhere classified Aerodynamics (excl. hypersonic aerodynamics) CFD aerodynamics Automotive Engineering not elsewhere classified Aerodynamics (excl. Hypersonic Aerodynamics) Computational Fluid Dynamics Gary Page Windsor Body 2.5 degree yaw unsteady CFD Simulation |
| title | Windsor Body 2.5 degree yaw unsteady CFD Simulation |
| title_full | Windsor Body 2.5 degree yaw unsteady CFD Simulation |
| title_fullStr | Windsor Body 2.5 degree yaw unsteady CFD Simulation |
| title_full_unstemmed | Windsor Body 2.5 degree yaw unsteady CFD Simulation |
| title_short | Windsor Body 2.5 degree yaw unsteady CFD Simulation |
| title_sort | windsor body 2.5 degree yaw unsteady cfd simulation |
| topic | Automotive engineering not elsewhere classified Aerodynamics (excl. hypersonic aerodynamics) CFD aerodynamics Automotive Engineering not elsewhere classified Aerodynamics (excl. Hypersonic Aerodynamics) Computational Fluid Dynamics |
| url | https://dx.doi.org/10.17028/rd.lboro.20089283.v1 |