Numerical modeling of hypersonic plasma
This grant funds developing computer models to understand the plasma layer forming around hypersonic vehicles, focusing on shockwaves and material interactions.
This grant is no longer accepting proposals
NRC Research Associateship Programs has archived this opportunity.
Funder: NRC Research Associateship Programs
Due Dates: May 1, 2025 (Naval Research Laboratory opportunity)
Funding Amounts: $99,200 stipend plus $3,000 travel allowance; relocation assistance available; typical fellowship duration 2-3 years
Summary: Supports postdoctoral research developing numerical models of hypersonic plasma and shock wave boundary layers at the Naval Research Laboratory.
Key Information: Open to U.S. citizens and permanent residents; requires Ph.D. earned within last 5 years; theoretical research focus on plasma physics, shock dynamics, and materials interactions in hypersonic flight.
Description
This fellowship opportunity at the Naval Research Laboratory (NRL) supports postdoctoral researchers in theoretical and computational studies of hypersonic flight phenomena. The research focuses on the complex interface layer between a hypersonic vehicle's surface and the plasma formed in contact with it, known as the hypersonic shock wave boundary layer. This plasma exists in a supersonic moving frame with steep gradients, producing shocks in accelerated non-equilibrium gases.
The goal is to develop advanced numerical codes and capabilities that address:
- Non-equilibrium plasma formation
- Shock wave dynamics
- Plasma chemistry under non-equilibrium conditions
- Materials physics related to vehicle surface interactions
- Radiation effects in the plasma environment
This research is fundamental to understanding and improving hypersonic vehicle design and performance.
