We are the Rotating Machinery Dynamics Section in the Fluid Machinery Department and Mechanical Engineering Division at SwRI. We design, develop, troubleshoot, and test new machinery for advanced power, oil & gas, and aviation applications.
Objectives of this Role:
Lead the design and analysis of Compressor and Turbine Aero Components for advanced machinery developed by the RMD section and lead reviews on designs provided by clients.
Perform 1D and 3D sizing and optimization of Aero geometry through CFD and other aero software/codes.
Utilize engineering software to conduct machinery flowpath development and analysis: Fluent, CFX, and Blade Generation software.
Lead test programs centered around Turbine and Compressor Aerodynamics.
Be a solution-oriented problem solver that exercises creativity and independent judgement in determining approaches to solve a wide range of technical problems with moderate supervision.
Write technical reports, papers, proposals and prepare technical presentations for client meetings and conferences.
Daily and Monthly Responsibilities:
Use engineering software for design and analysis of Turbine and Compressor Aero Components for use in advanced power, oil & gas, and aviation applications.
Perform engineering and scientific research and investigations to support projects in the industries of oil and gas, power generation, and aviation.
Project tasks will primarily be related to rotating machinery.
Provide analytical or experimental support to more than one project in a team environment, which can include literature reviews, data collection, test design, developing computational simulations, deriving first-principles or correlative based solutions to problems.
Interpret and present simulation results to project team and clients in a concise and clear way.
Interrogate results for reliability and provide troubleshooting support for tests and simulations with a firm understanding of theories and concepts using a first-principles approach.
Requirements:
Requires a Bachelors, Masters or a PhD in Mechanical Engineering, Aerospace Engineering or Electrical Engineering.
0-5 years: Experience or an interest in the Design and development of Turbine and/or Compressor Aero Components
If candidate has a graduate degree, prefer applicants whose degree program include academic experience in the design and development of radial and axial turbomachinery components.
Must be able to learn new technical skills to complete project work and develop custom tools to assist the team in future turbomachinery development work.
A valid/clear driver's license is required.
Special Requirements:
Must be a U.S. person (i.e., U.S. citizen, non-U.S. citizen national, lawful permanent resident, asylee, or refugee) due to ITAR work in section.
Job Locations: San Antonio, Texas
For more information about this division, visit the Mechanical Engineering home page.
For benefits information at our San Antonio location, click here. For benefits information at all other locations, click here.
An Equal Employment Opportunity/Affirmative Action Employer Race/Color/Religion/Sex/Sexual Orientation/Gender Identity/National Origin/Disabled/Veteran Committed to Diversity in the Workplace