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Hypersonic Aerothermodynamics Skill
Purpose
Provide specialized hypersonic vehicle aerodynamic and thermal analysis capabilities including real gas effects, aerodynamic heating, and thermal protection system design.
Capabilities
High-temperature gas dynamics
Real gas effects modeling
Aerodynamic heating prediction
Thermal protection system sizing
Shock-boundary layer interaction
Ablation modeling
Transition prediction (hypersonic)
Chemically reacting flow analysis
Usage Guidelines
Account for real gas and chemical non-equilibrium effects
Use appropriate turbulence models for hypersonic boundary layers
Predict transition location and heating augmentation
Size TPS with adequate margins for heating uncertainty
Consider ablation effects on aerodynamic shape
Validate predictions against ground test data where available
