Computation of hypersonic re-entry flow
This project presents a computational study of hypersonic reentry flow over a blunt body. Fluent™ computational fluid dynamics software will be used to simulate the flow over a cylinder in 2 different conditions. The first set of simulations involves reentry flow at 65km at a Mach number of 22. The...
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| Format: | Final Year Project |
| Language: | English |
| Published: |
2013
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| Online Access: | http://hdl.handle.net/10356/54646 |
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| Institution: | Nanyang Technological University |
| Language: | English |