Drag reduction on a transonic airfoil
DOI10.1017/JFM.2022.369zbMath1495.76061arXiv2204.12172OpenAlexW4280529503MaRDI QIDQ5077738
Jacopo Banchetti, A. Chiarini, Davide Gatti, Maurizio Quadrio, Antonio Memmolo, Sergio Pirozzoli
Publication date: 19 May 2022
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Full work available at URL: https://arxiv.org/abs/2204.12172
direct numerical simulationcompressible Navier-Stokes equationscalorically perfect gassecond-order energy-consistent finite volume methodshock wave effectturbulent skin-friction drag reduction
Shock waves and blast waves in fluid mechanics (76L05) Transonic flows (76H05) Finite volume methods applied to problems in fluid mechanics (76M12) Direct numerical and large eddy simulation of turbulence (76F65) Flow control and optimization for compressible fluids and gas dynamics (76N25) Control of turbulent flows (76F70) Compressible Navier-Stokes equations (76N06)
Cites Work
- Boundary conditions for direct simulations of compressible viscous flows
- Large-eddy simulation of the shock/turbulence interaction
- Assessment of spanwise domain size effect on the transitional flow past an airfoil
- Turbulent boundary layers at moderate Reynolds numbers: inflow length and tripping effects
- Streamwise-travelling waves of spanwise wall velocity for turbulent drag reduction
- Mechanisms for generating coherent packets of hairpin vortices in channel flow
- Critical assessment of turbulent drag reduction through spanwise wall oscillations
- Separation drag reduction through a spanwise oscillating pressure gradient
- Reynolds-number dependence of turbulent skin-friction drag reduction induced by spanwise forcing
- Turbulent drag reduction over curved walls
- Supersonic turbulent boundary layer drag control using spanwise wall oscillation
- Shock Wave Drag Reduction
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