TITLE : PHOENICS IN THE AEROSPACE INDUSTRY : GAS TURBINE ENGINE TEST CELL

BY : CHAM Consultancy Team
FOR : Industrial Client
DATE : 1991
PHOENICS Version : 1.6

DETAILS :

• Three-Dimensional incompressible steady flow
• Curvilinear(BFC) computational grid

NOTES :

• The gas-turbine cell comprises of an inlet section, test section, exhaust duct and exit section
• The engine is suspended from the test section roof. Its geometry consists of a bell-nozzle which captures the required airflow

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