Rao, SVR and Khosla, S (2002) Numerical analysis of transpiration cooling in carbon dioxide atmosphere at hypersonic Mach numbers. In: 2nd International Conference on Computational Fluid Dynamics, JUL 15-19, 2002, Sydney, Australia.Full text not available from this repository.
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.
|Item Type:||Conference Paper|
|Additional Information:||Copyright of this article belongs to Springer-Verlag Berlin.|
|Department/Centre:||Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)|
|Date Deposited:||16 Mar 2012 12:23|
|Last Modified:||16 Mar 2012 12:23|
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