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Research Engineer – Combustion

Research Engineer – Combustion

CompanyGE Aerospace
LocationSchenectady, NY, USA
Salary$80000 – $150000
TypeFull-Time
DegreesMaster’s, PhD
Experience LevelSenior

Requirements

  • Doctorate in Mechanical Engineering, Aerospace Engineering or related disciplines OR Master’s degree in Mechanical Engineering, Aerospace Engineering or related disciplines with at least 5 years of relevant experience
  • Knowledge of combustion, acoustics, thermodynamics, hydrodynamics, and combustion chemistry
  • Experience with post-processing computational and/or experimental data
  • Background in advanced mathematics (numerical methods, pde/ode, etc.)
  • Experience in performing combustion experiments
  • Demonstrated ability to investigate, model and provide critical insight into complex physical phenomena
  • Ability to work effectively in a multidisciplinary team
  • Excellent communication skills and ability to interface with senior leaders and customers with clarity and confidence
  • Must be willing to work out of an office located in Niskayuna, NY
  • U.S. citizenship is required due to Federal Contract Provisions

Responsibilities

  • Work with technicians and engineers to design and install new experimental hardware
  • Perform high-pressure combustion experiments simulating engine operation and analyze data
  • Contribute to project reviews and archive results – recommend design improvements
  • Work with other engineers in developing new combustion models and analysis tools
  • Lead cutting edge research in turbine engine combustion and high-speed propulsion
  • Work as part of a team executing on multi-generation technology programs to enable future design advancements

Preferred Qualifications

  • Background in gas turbine combustion, including: thermo-acoustic instabilities (combustion dynamics), fuel/air premixing systems, flame propagation in complex fuel mixtures, combustion kinetics & chemistry, design and evaluation of new combustion systems, and modeling of combustion systems
  • Experience with advanced instrumentation and optical diagnostics
  • Experience in modeling supersonic/hypersonic flows
  • Peer reviewed journal publications
  • Experience working with high-pressure, high-temperature combustion experiments
  • Fluency with Matlab, Python, and COMSOL