Fixed-support conditions are applied on the bottom of the disk portion of the model:
The following loads are considered:
Centrifugal loads caused by rotational velocity
Thermal loads due to the difference in reference and operating temperature
Unsteady flow pressure applied on the fan blade
The rotational velocity (CGOMGA,0,0,1680) is applied along the global Z axis. The reference temperature is maintained at 22°C, and the temperature loading is applied on the blade (BF):
The unsteady flow pressures (imported from Ansys CFX) are generated for EO = 2 engine-order excitation at a rotational frequency of 534.76 Hz. The pressure data are then mapped to the structural rotor fan blade model in Mechanical APDL via its mapping processor (/MAP).