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 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
PhD research proposal PhD work planning Intro Multimodel ROM Mesh Implicit Thermo Research project Purpose of the research Accelerate and improve the efficiency and accuracy of high-fidelity computational aeroservoelastic analysis Developments towards a faster CAE based loads analysis process: Variable fidelity multimodel multidomain coupling approach New reduced order modelling techniques Mesh motion enhancements Implicit solver for CFD Thermal solver for aerothermoelasticity Accuracy/fidelity Area of interest Potential Methods Euler Methods Navier-Stokes Methods Computational resources (cost/time) Matteo Ripepi Fast high-fidelity aero-servo-thermo-elastic analysis
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A Framework for Fast CFD-based Aero-Servo-Thermo-Elastic Analysis

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