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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 />

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

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