Shock-boundary layer interaction and transition modelling in turbomachinery flows

Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy

Volumn 211, Issue 3, 1997, Pages 225-234

  Michelassi, V ^a  

^a UNIVERSITY OF FLORENCE   (Italy)

Author keywords

Numerical methods; Shock boundary layer interaction; Transition models; Transonic flows; Turbulence models

Indexed keywords

BOUNDARY LAYERS; CASCADES (FLUID MECHANICS); CHANNEL FLOW; COMPRESSIBLE FLOW; COMPUTATIONAL FLUID DYNAMICS; FLOW INTERACTIONS; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; SHOCK WAVES; TRANSONIC FLOW; TURBOMACHINE BLADES; TURBULENCE;

SHOCK BOUNDARY LAYER INTERACTION; STAGNATION POINTS; TURBULENCE MODEL;

TURBOMACHINERY;

BOUNDARY LAYER; MATHEMATICAL MODELING; SHOCK WAVE; TURBOMACHINERY;

EID: 0141869657     PISSN: 09576509     EISSN: None     Source Type: Journal    
DOI: 10.1243/0957650971537132     Document Type: Article

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