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

Data in Brief

Valentina Motta¹  Alessia Laforì²  Maria Grazia De Giorgi³  Antonio Suma⁴ 

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

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

DOI  :  

来源: DOAJ

【 摘 要 】

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.

【 授权许可】

Unknown