Numerical analysis of a divergent duct with high enthalpy transonic cross injection
In the present study, an aerothermodynamic analysis of high-speed flow fields through a divergent duct (similar to a supersonic combustor: hereafter referred to as supersonic combustor in the paper), without injection and with high enthalpy cross injection, has been performed. Initially, the thermal...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
MULTIPHYSICS
2016-09-01
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| Series: | International Journal of Multiphysics |
| Online Access: | http://journal.multiphysics.org/index.php/IJM/article/view/191 |