
Explore how aerodynamic, thermal, structural, and manufacturing conditions influence the performance of aircraft and space systems. Connect your computational models and experimental data with Physics Intelligence in a solution customized to compare designs and operating scenarios.
Evaluate changes in pressure, aerodynamic loading, and heat transfer across geometries and flow conditions. Explore design alternatives that address aerodynamic performance and thermal requirements across operating scenarios.
Evaluate temperature changes and thermal stress across sunlit and shaded conditions, accounting for solar radiation, planetary or surface infrared radiation, and conduction through structures. Compare geometry, thermal contacts, and material absorptivity and emissivity to explore thermally stable designs and operating conditions for spacecraft and lunar surface vehicles.
Evaluate vibration and acoustic responses across excitation, geometry, and operating conditions. Examine relationships among resonance, vibration transmission, and noise generation to compare designs against dynamic performance targets.
Evaluate how material flow, thermal history, and deformation during manufacturing influence final geometry and physical behavior. Compare material and process choices to explore designs that address dimensional stability and mechanical performance together.
