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
Solid 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.