Talascend is currently seeking a Gas Turbine Performance Engineer for a contract opportunity with our client in Phoenix, Arizona.
Overview
This role involves performing thermodynamic modeling and analysis of aerospace gas turbine engines, with a focus on steady state and transient performance and operability. The engineer will build, debug, and refine NPSS engine cycle models and support requirements analysis and data reduction to aid engine development and qualification.
Responsibilities
- Build, debug, refine, and maintain steady state and transient thermal models using NPSS (Numerical Propulsion System Simulation)
- Develop NPSS customer models
- Foster productive knowledge transfer of NPSS modeling techniques
- Perform requirements analysis and requirements decomposition
- Provide test coverage and data reduction to support engine development and qualification
- Communicate effectively to leadership, customers, and peers including presentations and technical reports
- Work collaboratively across cross-functional disciplines and teams
Qualifications
- Bachelor's degree from an accredited institution in a technical discipline such as sciences, technology, or engineering
- 4 years of experience with turbine engine Performance & Operability Modeling and Analysis
- Demonstrated ability to perform the duties of this position through relevant experience, training, or education
- U.S. citizen
We thank all applicants for their interest. However, only those qualified individuals who closely meet the qualifications of the position will be contacted. The details of the position are only a summary, other duties may be assigned as necessary.
Background Check and Drug Screen may be required.
Talascend is an Equal Opportunity Employer that recruits and hires qualified candidates without regard to race, religion, sex, sexual orientation, gender identity, age, national origin, ancestry, citizenship, disability, or veteran status.