Study of Non-Equilibrium Flow Behind Normal Shock
Normal shock problems in high enthalpy flows are of special interests to aerodynamicists and fluid dynamicists. When the shock Mach number become hypersonic and increasing further, the gas passing through the shock is compressed resulting in increase in temperature and pressure. As the Mach number i...
| Main Author: | |
|---|---|
| Other Authors: | |
| Language: | en_US |
| Published: |
2017
|
| Subjects: | |
| Online Access: | http://etd.iisc.ernet.in/handle/2005/2891 |