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...
Main Author: | Lee, Choon Yee. |
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Other Authors: | Chue Shek Ming Randy |
Format: | Final Year Project (FYP) |
Language: | English |
Published: |
2013
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Subjects: | |
Online Access: | http://hdl.handle.net/10356/54646 |
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