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RESEARCH ENGINEER - SR. RESEARCH ENGINEER - High-speed Air Breathing Propulsion/Aero

SWRI
San Antonio, TX Full Time
POSTED ON 3/3/2025
AVAILABLE BEFORE 5/28/2025
  • Support the development, analysis, and testing of systems related to experimental and numerical modeling of supersonic and hypersonic flows, focusing on airbreathing propulsion components.
  • Engage in the design and operation of sophisticated test rigs for supersonic and hypersonic experiments, contributing to advanced research in aerodynamics, thermodynamics, and propulsion.
  • Apply knowledge in high-speed fluid dynamics, shock wave interactions, boundary layer theory, and combustion processes to optimize designs and enhance performance in propulsion systems.
  • Utilize state-of-the-art Computational Fluid Dynamics (CFD) software such as Ansys Fluent, STAR-CCM , and OpenFOAM to simulate flow conditions and analyze aerothermal loads affecting vehicles and components at high Mach numbers.
  • Integrate experimental insights with simulation data to validate models and develop predictive capabilities for propulsion systems operating in extreme environments.
  • Provide cross-disciplinary support to multiple projects within the field of high-speed aerodynamics, focusing on both computational and experimental tasks.
  • Conduct design, optimization, and validation of high Mach number flow regimes using both CFD and experimental techniques.
  • Contribute to the design and commissioning of supersonic and hypersonic test facilities, including facility upgrades and instrumentation enhancements.
  • Assist in the execution of experimental test campaigns, including data acquisition, processing, and analysis to support model validation.
  • Be a problem solver that exercises creativity and independent judgement in determining approaches to solve a wide range of technical problems.
  • Requires a Bachelors, Masters or a PhD in Mechanical Engineering, Aerospace Engineering, Chemical Engineering, or related engineering degree. 1 year experience require with MS degree, 0 years experience required with PhD in relevant areas.
  • 2-5 years : Experience in high-speed aerodynamics, including both experimental and CFD modeling, particularly regarding supersonic / hypersonic flows. Demonstrated experience in either experimental OR numerical work in supersonics or hypersonics. Experience in both preferred, but not required.
  • 2-5 years : Experimental : design, operation, and troubleshooting of supersonic and hypersonic test facilities like continuous, blowdown, shock tubes, Ludweig tubes, arc-jet tunnels, etc. Subsonic wind tunnel experience also considered.
  • 2-5 years : Numerical : Proven ability in using CFD software such as Ansys Fluent, STAR-CCM , or OpenFOAM for high-speed aerodynamic simulation and analysis. Unsteady, reacting flow, multiphase, and fluid-structure interaction experience also considered.
  • Experience with combustion processes and the design of subsonic or supersonic combustors is highly desirable but not mandatory. MS or PhD degrees in engineering are preferred, but not required.
  • A valid / clear driver's license is required.
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