Exploration of plasma-based control for low-Reynolds number airfoil/gust interaction

DOI10.1080/10618562.2011.632374zbMath1271.76299OpenAlexW2091927701MaRDI QIDQ2847532

Miguel R. Visbal, Donald P. Rizzetta

Publication date: 10 September 2013

Published in: International Journal of Computational Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/10618562.2011.632374

zbMATH Keywords

large-eddy simulationgustlow-Reynolds number airfoilplasma-flow controlvortex/airfoil interaction

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Flow control and optimization for compressible fluids and gas dynamics (76N25) Ionized gas flow in electromagnetic fields; plasmic flow (76X05)

Related Items (1)

Rankine combined vortex interaction with a rectangular prism

Uses Software

• FDL3DI

Cites Work

• A diagonal form of an implicit approximate-factorization algorithm
• Compact finite difference schemes with spectral-like resolution
• High-order compact finite-difference methods on general overset grids
• Strategies for control of transitional and turbulent flows using plasma-based actuators
• VERY HIGH-ORDER SPATIALLY IMPLICIT SCHEMES FOR COMPUTATIONAL ACOUSTICS ON CURVILINEAR MESHES
• An approximate deconvolution procedure for large-eddy simulation
• An explicit filtering method for large eddy simulation of compressible flows
• An Implicit Factored Scheme for the Compressible Navier-Stokes Equations
• Numerical simulation of delta-wing roll
• A time-implicit high-order compact differencing and filtering scheme for large-eddy simulation
• On the identification of a vortex
• Validation of the RANS-simulation of laminar separation bubbles on airfoils

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