TITLE : GAS TURBINE ROTOR BLADE

BY : CHAM Consultancy Team - J P Edwards
DATE : 1992 PHOENICS Version : 1.6

DETAILS :

• Three-Dimensional Steady compressible flow
• Curvilinear (BFC) H-Type Computational grid with blockage

NOTES :

• Simulation of the flow in a first stage gas-turbine rotor
• Rotor blade considered with the following parameters : a. Variable aerofoil section b. Taper c. Twist

  Pictures are as follows :
  Computational Grid
  Velocity Vectors
  Pressure Contours
  

  wbs