Data-Driven Modelling of Compressor Stall Flutter

Lead Research Organisation: Imperial College London
Department Name: Mechanical Engineering

Abstract

In this project we have applied data-driven techniques for the computations of aerodynamic damping of turbomachinery, which is a first application of such approaches to this topic. The outcome of this project can be used by aero-engine designers to assess flutter stability at design.

Publications

10 25 50

Studentship Projects

Project Reference Relationship Related To Start End Student Name
EP/R513052/1 01/10/2018 30/09/2023
2899868 Studentship EP/R513052/1 01/10/2018 30/09/2020 Marco Rauseo