Physics Based Models for Power and Propulsion Innovations using High Performance Computing
Not specified
No deadline
United States
individual
About This Opportunity
The US Army Research Laboratory, Mechanical Sciences Division, conducts basic and applied research in Turbine Power and Propulsion to address far-term science and technology challenges that are envisioned for the future battlefield environment in Multi-Domain Operations (MDO). This research associateship is a critical part of on-going mission programs towards developing innovative propulsion technologies, including adaptive turbine propulsion, pressure gain combustion, and morphing hypersonic systems for current and future Army vehicles. This research will focus on the development of new physics based computational fluid dynamic models to be deployed on DoD leadership High Performance Computing (HPC) facilities leveraging exceptional resources and teaming with internal and cross-directorate experts in mechanical and computational sciences. This position will also involve collaborations with leading OEMs and academia. The models developed will have direct links to experimental facilities at ARL Weapons and Materials Research Directorate as well as external facilities for validation and concept vetting efforts. Research proposals are invited that advance first principle and engineering models for compressible fluid-dynamics, particle-laden turbulence, fluid structure interactions, and conjugate heat transfer, including Direct Numerical Simulation (DNS), Large Eddy Simulation (LES), or RANS approaches.
Who Can Apply
- Region
- United States
- Citizenship
- United States
- Project in
- United States
- Applicants
- individual
- Age
- 18 - 151 years old
Application Details
Stages
- 1 two_stage
Required documents
Review process
Initial selection by advisor followed by research proposal submission to ARL-RAP review panel
Additional benefits
- mentorship
- networking
- equipment
External Application
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- Award Amount
- Not specified
- Application Deadline
- No deadline
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