15 - Guest lectures

AERO-THERMO-STRUCTURAL OPTIMIZATION OF INTEGRATED THERMAL PROTECTION SYSTEMS

M. Santer, Imperial College London, United Kingdom

Hypersonic vehicles have many critical components that are exposed to large aerothermal heat fluxes and extreme temperatures. Their design is challenging as structural and aero-thermal requirements are often in opposition. To address this, topology optimization of these components, in particular integrated thermal protection systems, will be demonstrated accounting for their transient thermoelastic response, and a range of multidisciplinary system-level constraints.

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