Numerical and Experimental Analysis of Transpiration Cooling in Carbon Dioxide Atmosphere at Hypersonic Mach Numbers
INDIAN INST OF SCIENCE BANGALORE DEPT OF AEROSPACE ENGINEERING
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The numerical solutions are obtained for skin friction, heat transfer to the wall and growth of boundary layer along the flat plate by employing two dimensional Navier-Stokes equations governing the hypersonic flow coupled with species continuity equations. Flow fields have been computed along the flat plate in CO2 atmosphere in the presence of transpiration cooling using air and carbon dioxide.
- Numerical Mathematics
- Fluid Mechanics