Dataset of numerical simulations for aeroelastic control of an aero engine compressor cascade using plasma actuators

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.

Keywords

• Load alleviation
• Cascade
• Flutter
• AC-DBD plasma
• Flow control
• Unsteady flow