Aerodynamic Design Engineer

LTTS · Bangalore

Collected role description

Aerodynamic Design Engineer at LTTS

Carry out gas turbine turbomachinery aerodynamic design and analysis activities.

This role requires expert knowledge in gas turbine propulsion, planning for projects and ability to develop individuals.

Carry out design & off-design analysis, post-process engine test data, liaise with internal and external stakeholders.
Provide technical leadership in engine architectural studies
Develop numerical and experimental methods for method verification and validation
Define individual and team performance metrics, monitor the performance, and provide constructive feedback
Review the designs, simulations and generate testing guidelines
Identify project risks and plan for mitigation Qualifications &

Aerospace, Mechanical Engineering degree or a related field.
Strong background in gas turbine propulsion, turbomachinery design, thermodynamics and fluid mechanics.
Hands-on experience in axial and centrifugal compressor, turbine design and optimization for gas turbine applications.
Experience in unsteady modelling, bleed flows, compressor stability, casing treatment and sub-idle modelling will be considered as plus.
Fluent in English
5-15 years or more.
Skills

in one or a combination of stated topics.
Using commercial turbomachinery tools such as Concepts NREC, AxStream or similar.
Experience in CFD or through flow simulation methods.
Ansys CFX, Numeca/Cadence, Fluent etc.
Experience in multi-point and multi-disciplinary optimization
Experience in programming using C, Matlab/Simulink or similar.
Experience in coatings, and cooling technologies.
Awareness on the state-of-the-art technologies in materials, heat transfer and structural mechanics to link with aerodynamic design and performance
Good communication and presentation skills to interact with team members, clients, and vendors.
Ability to solve problems, prioritize tasks and delegate when necessary

Aerodynamics engineer will be responsible for carrying out the gas turbine turbomachinery design and analysis activities within the turbojet and turbofan development programs.

5-15 years