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

PhD research proposal PhD work planning Intro Multimodel ROM Mesh Implicit Thermo
Computational aeroservoelasticity
Load factor
3
2
1
0
Loads database prediction
Flaps Down
is fundamental in the overall aircraft design and development
involves a large amount of aeroelastic analyses
Flaps Up
CFD mostly done
near cruise point
VEAS
High-fidelity computational aeroservoelasticity
still too computationally expensive for the preliminary design stage,
and therefore used for a limited number of cases (e.g. flutter).
high potential for the prediction of critical flight loads
necessary to address new challenges in aircraft design
Matteo Ripepi Fast high-fidelity aero-servo-thermo-elastic analysis