Analysis of Material Behavior for Friction in a Nozzle for Turbomachinery and High Speed Vehicles

S. M. Prabhu, Abbas Mohadeen

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DOI: 10.4236/msa.2011.210200                

Abstract

Shock-induced separation of turbulent boundary layers represents a long-studied problem in compressible flow, bearing, for example, on applications in high speed aerodynamics, rocketry, wind tunnel design, and turbomachinery. Experimental investigations have generally sought to expose essential physics using geometrically simple configurations.

Keywords

Adiabatic Proces, Friction Efects, Nozzle Modeling, Materialbehavior

Conflicts of Interest

The authors declare no conflicts of interest.

References

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