Comparison Study on Different Compressibility Modifications of Turbulence Model in Supersonic Combustion Simulation
Supersonic combustion in two-model scramjet combustors of hydrogen and hydrocarbon fuel was, respectively, simulated using the in-house two-dimensional compressible, turbulent, and reacting flow code. Three kinds of compressibility modifications, namely, the dilatational compressibility, structural...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
SAGE Publishing
2014-02-01
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| Series: | Advances in Mechanical Engineering |
| Online Access: | https://doi.org/10.1155/2014/238250 |