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

Maria Grazia De Giorgi; Valentina Motta; Antonio Suma; Alessia Laforì

doi:10.1016/j.dib.2021.107584

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

Data Brief. 2021 Nov 16:39:107584. doi: 10.1016/j.dib.2021.107584. eCollection 2021 Dec.

Authors

Maria Grazia De Giorgi¹, Valentina Motta², Antonio Suma¹, Alessia Laforì¹

Affiliations

¹ Department Engineering for Innovation, University of Salento, Via per Monteroni, 73100 Lecce, Italy.
² General Electric, Advanced Technology & Sciences, Franklinstraße 14, 10587 Berlin, Germany.

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: AC-DBD plasma; Cascade; Flow control; Flutter; Load alleviation; Unsteady flow.