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 />
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