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Updated: Oct 11, 2025

A Modeling and Simulation Method for Preliminary Design of an Electro-Variable Displacement Pump
Published on: June 1, 2022
Dataset of numerical simulations for aeroelastic control of an aero engine compressor cascade using plasma actuators
Maria Grazia De Giorgi1, Valentina Motta2, Antonio Suma1
1Department Engineering for Innovation, University of Salento, Via per Monteroni, 73100 Lecce, Italy.
Abstract:
The dataset presented here regard the analysis reported in the research article entitled "Comparison of different plasma actuation strategies for aeroelastic control on a linear compressor cascade" De Giorgi et al. (2021) [1]. These data are related to the Computational Fluid Dynamics (CFD) assessment of different plasma actuation strategies for the aeroelastic control of an aero engine compressor cascade in subsonic flow conditions. The authors evaluated the accuracy of numerical computations using experimental results. Here, both experimental and raw data of the CFD simulations are presented.
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