Advance detonation engine inlet research using computational fluid dynamics and experimental validation in a supervised laboratory fellowship. The work targets attritable UAS propulsion.
This two-year postdoctoral fellowship develops and evaluates a novel inlet architecture for detonation engines. Research combines computational fluid dynamics, experimental validation, and compressible-flow knowledge to assess feasibility. The project addresses low-cost, high-efficiency propulsion systems for attritable uncrewed aerial systems.
Key Responsibilities:
- Develop novel inlet architectures for detonation engines
- Evaluate proposed inlet designs through computational fluid dynamics
- Conduct experimental validation of research findings
- Establish feasibility of detonation engine inlets
- Work under direct supervision of an NRC researcher
Requirements:
- PhD in Mechanical or Aerospace Engineering
- Basic experience in additive manufacturing design
- Basic experience using advanced cooling technologies
- Basic experience in compressible flow
- English language proficiency and Reliability Status eligibility
Apply detonation, compressible-flow, computational, and experimental expertise to low-cost propulsion research for attritable UAS.