Development of Ab Initio Collision Models for Direct Simulation Monte Carlo Simulations of Hypersonic Flows
| dc.contributor.author | Mallick, Ashirbad | |
| dc.date.accessioned | 2026-10-21T11:11:26Z | |
| dc.date.issued | 2026 | |
| dc.description | Mankodi, Tapan Krishnakumar | |
| dc.description.abstract | Direct Simulation Monte Carlo (DSMC) is a widely used numerical technique for simulating rarefied gas flows encountered in aerospace and micro-scale engineering applications, such as atmospheric re-entry, hypersonic flight, vacuum systems, and microchannel flows. The method provides a probabilistic solution to the Boltzmann equation by tracking the motion and collisions of representative particles. It has become one of the most reliable approaches for studying non-equilibrium gas dynamics. The accuracy of DSMC simulations, however, strongly depends on the collision models employed to represent intermolecular interactions and transport processes. | |
| dc.identifier.other | ROLL NO.206103106 | |
| dc.identifier.uri | https://gyan.iitg.ac.in/handle/123456789/3615 | |
| dc.language.iso | en | |
| dc.relation.ispartofseries | TH-4144 | |
| dc.rights | https://creativecommons.org/licenses/by-nc-sa/4.0/ | |
| dc.rights.uri | https://creativecommons.org/licenses/by-nc-sa/4.0/ | |
| dc.subject | MECHANICAL ENGINEERING | |
| dc.title | Development of Ab Initio Collision Models for Direct Simulation Monte Carlo Simulations of Hypersonic Flows | |
| dc.type | Thesis |
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