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 />
New reduced order modelling techniques<br />
ROM requires a set of instantaneous flow solutions (snapshots)<br />
Projection of onto a reduced subspace<br />
Direct identification of a system of the required <strong>for</strong>m<br />
Hilbert-Huang Trans<strong>for</strong>m decomposition of aeroelastic system<br />
adaptive data analysis <strong>for</strong> nonlinear and nonstationary processes.<br />
Subspace-<strong>based</strong> identification methods<br />
identify a state-space model directly from input-output data<br />
Global aeroelastic ROM<br />
parametric input space<br />
interpolation of flight data<br />
(full/low order simulations)<br />
Polinomial response surface<br />
Kriging/Co-Kriging<br />
Matteo Ripepi <strong>Fast</strong> high-fidelity aero-servo-thermo-elastic analysis