Turbine & Hot Gas Path Aero Engineer

📋 Description

• Design, test, and evaluate turbine components aerodynamics.
• Mean-line and quasi-3D aerodesign using through-flow tools.
• High-fidelity 3D CFD simulations to assess turbine performance.
• Blade geometry optimization to meet aero and structural targets.
• Hot-section interpretation: combustor exit conditions and temp non-uniformity.

🎯 Requirements

• Master’s degree in Aerospace/Mechanical Eng with turbomachinery/aero/thermal focus.
• 3+ years in turbine aerodynamics or hot-gas-path work.
• Strong turbomachinery aerodynamics, loss modelling, and flow physics.
• Advanced 3D CFD (CFX) for turbomachinery flow analysis and evaluation.
• Strong capability in mean-line/throughflow/2D blade analyses.
• Experience in blade shape optimization.
• Solid foundation in heat transfer, compressible flow, thermodynamics.
• Proficient in CAD software (NX or equivalent).

🎁 Benefits

• Core team opportunity at a high-conviction deep-tech startup
• Build next-gen India GTEs
• Fast-paced hardware environment with ownership and impact