Direct computations of boundary layers distorted by migrating wakes in a linear compressor cascade

Flow, Turbulence and Combustion

Volumn 83, Issue 3, 2009, Pages 307-322

  Zaki, T A ^a   Wissink, J G ^b   Durbin, P A ^c   Rodi, W ^d  

^a IMPERIAL COLLEGE LONDON   (United Kingdom)

^b BRUNEL UNIVERSITY   (United Kingdom)

^c Iowa State University of Science and Technology   (United States)

^d UNIVERSITY OF KARLSRUHE   (Germany)

Author keywords

Bypass transition; Compressor; Separation; Wakes

Indexed keywords

ARMED FORCES; BYPASS TRANSITION; COMPRESSOR CASCADE; CYLINDER DIAMETERS; GRID POINTS; INFLOW VELOCITY; KELVIN-HELMHOLTZ INSTABILITIES; LINEAR COMPRESSORS; PRESSURE SURFACE; SUCTION SURFACES; TRANSITION TO TURBULENCE;

ATMOSPHERIC THERMODYNAMICS; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; CIRCULAR CYLINDERS; COMPRESSORS; COMPUTATIONAL GEOMETRY; COMPUTER SIMULATION; FLOW SIMULATION; INCOMPRESSIBLE FLOW; INTERNET PROTOCOLS; REYNOLDS NUMBER; SEPARATION; TURBULENCE;

WAKES;

EID: 70349656439     PISSN: 13866184     EISSN: 15731987     Source Type: Journal    
DOI: 10.1007/s10494-009-9216-0     Document Type: Article

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