Novel flow control method for vortex shedding of turbine blade

Transactions of the Japan Society for Aeronautical and Space Sciences

Volumn 53, Issue 180, 2010, Pages 122-129

  El Gend, Mahmoud M ^a   Ibrahim, Mohammed K ^a,b   Mor, Koichi ^a   Nakamura, Yoshiaki ^a  

^a NAGOYA UNIVERSITY   (Japan)

^b CAIRO UNIVERSITY   (Egypt)

Author keywords

CFD; Flow control; Microtubes; Turbine blade; Vortex shedding

Indexed keywords

BASE PRESSURE; DELAYED-DETACHED EDDY SIMULATION; DUAL TIME METHOD; FLOW CONTROL METHODS; FLUX DIFFERENCE SPLITTING; ISENTROPIC; MICROTUBES; NUMERICAL CODE; NUMERICAL FLUX; SIMULATED RESULTS; SUCTION SIDE; THREE-DIMENSIONAL FLOW; TIME INTEGRATION; TRAILING EDGES; TURBINE BLADE; TURBINE CASCADE;

CASCADES (FLUID MECHANICS); FLOW CONTROL; MACH NUMBER; NUMERICAL METHODS; REYNOLDS NUMBER; TURBINES; VORTEX FLOW; VORTEX SHEDDING;

TURBOMACHINE BLADES;

EID: 80052474679     PISSN: 05493811     EISSN: None     Source Type: Journal    
DOI: 10.2322/tjsass.53.122     Document Type: Review

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