Role: Work on the rotordynamic design and analysis of high-speed turbomachinery for indigenous micro turbojet engines.
Key Responsibilities:
Rotor-bearing system modelling and analysis.
Critical speed, Campbell diagram, and rotor stability analysis.
Vibration analysis and agile response assessment.
Support rotor design optimisation and experimental validation.
Requirements:
Robust fundamentals in rotordynamics and vibration mechanics.
Experience with ANSYS or equivalent simulation tools.
Knowledge of high-speed turbomachinery is preferred.
Ideal Candidate: A hands-on engineer passionate about solving challenging engineering problems in aerospace propulsion.