We provide computational support for hypersonic research focused on control surface thermal management and propulsion system structural integration — including fluid-structure interaction (FSI), material response to heating and pressure through ablation, and fluid dynamics at high Mach numbers.

We develop advanced material solutions for vehicle and hypersonic applications, targeting improved structural and thermal properties. Our ICME approach is often paired with multiple optimization regimes to efficiently identify the most promising solutions.

We optimize product geometry to reduce weight or improve flow characteristics while maintaining — or improving — performance. Paired with material optimization and ICME, this lets us rapidly build virtual prototypes of complex systems within strict space and performance requirements.