Raj_Aron
Aerospace
- Oct 6, 2016
- 5
As part of my thesis, I have carried out modal analysis of a compressor rotor blade with and without fouling mass accumulation and plotted this on a Campbell diagram as shown.
Only considering the design rpm case, I have tried to simulate the blade vibration amplitudes using harmonic response on ansys workbench using the force exerted by the gas on the blade. But I want to implement the excitation frequencies (multiples of running frequency from campbell diag.) into the model and see the effect on blade vibration amplitudes. Is this possible?

Only considering the design rpm case, I have tried to simulate the blade vibration amplitudes using harmonic response on ansys workbench using the force exerted by the gas on the blade. But I want to implement the excitation frequencies (multiples of running frequency from campbell diag.) into the model and see the effect on blade vibration amplitudes. Is this possible?