Numerical simulation over a multi-body launch vehicle module at various transonic Mach numbers
Simulations have been carried out for a multi-body launch vehicle configuration using CFD code 'PARAS-3D'. PARAS-3D is a Reynolds Averaged Navier Stokes equations (RANS) solver with k-ε turbulence model. The transonic regime is a critical regime for any launch vehicle configuration because...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
University of Belgrade - Faculty of Mechanical Engineering, Belgrade
2017-01-01
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| Series: | FME Transactions |
| Subjects: | |
| Online Access: | https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2017/1451-20921701009R.pdf |