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A Framework for Fast CFD-based Aero-Servo-Thermo-Elastic Analysis

A Framework for Fast CFD-based Aero-Servo-Thermo-Elastic Analysis

A Framework for Fast CFD-based Aero-Servo-Thermo-Elastic Analysis

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PhD research proposal PhD work planning Intro Multimodel ROM Mesh Implicit <strong>Thermo</strong><br />

Research project<br />

Thermal solver <strong>for</strong> aerothermoelasticity<br />

Thermal solver <strong>for</strong> <strong>CFD</strong>-<strong>based</strong> aerodynamic heating<br />

aero-thermo-elasticity<br />

hypersonic aeroelastic stability problems<br />

aeroelastic analysis that accounts <strong>for</strong> the effect of thermal<br />

stresses and material degradation.<br />

<strong>Aero</strong>thermoelasticity will also take advantage of ROM tecniques.<br />

q aero<br />

q strd<br />

q cond<br />

q rad<br />

wing<br />

structure<br />

Exposed<br />

surface/TPS<br />

Control<br />

Heat<br />

transfer<br />

<strong>Aero</strong>dynamic<br />

<strong>for</strong>ces<br />

Structural<br />

displacements<br />

Matteo Ripepi <strong>Fast</strong> high-fidelity aero-servo-thermo-elastic analysis<br />

Inertial<br />

effects

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