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Analysis of Material Behavior for Friction in a Nozzle for Turbomachinery and High Speed Vehicles
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Materials Sciences and Applications·Volume 02 (2011)·Pages 1485–1490·Published 18 October 2011·DOI10.4236/msa.2011.210200
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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.
KeywordsAdiabatic ProcesFriction EfectsNozzle ModelingMaterialbehavior
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