Wall-cooling effects on pressure fluctuations in compressible turbulent boundary layers from subsonic to hypersonic regimes

DOI10.1017/jfm.2022.595zbMath1494.76050OpenAlexW4289519772WikidataQ113858309 ScholiaQ113858309MaRDI QIDQ5094690

Peng-Jun-Yi Zhang, De-jun Sun, Nan-Sheng Liu, Zhen-Hua Wan, Xi-Yun Lu

Publication date: 4 August 2022

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/jfm.2022.595

zbMATH Keywords

direct numerical simulationcompressible boundary layerhigh-order finite difference methodpressure fluctuationacoustic modevorticity mode

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Direct numerical and large eddy simulation of turbulence (76F65) Turbulent boundary layers (76F40) Hypersonic flows (76K05) Compressibility effects in turbulence (76F50)

Related Items (5)

Linear response analysis of supersonic turbulent channel flows with a large parameter space ⋮ Conditional analysis on extreme wall shear stress and heat flux events in compressible turbulent boundary layers ⋮ Wall cooling effect on spectra and structures of thermodynamic variables in hypersonic turbulent boundary layers ⋮ Reynolds number and wall cooling effects on correlations between the thermodynamic variables in hypersonic turbulent boundary layers ⋮ Effect of bulk viscosity on the hypersonic compressible turbulent boundary layer

Cites Work

• Unnamed Item
• Spectral methods for the Navier-Stokes equations with one infinite and two periodic directions
• Boundary conditions for direct simulations of compressible viscous flows
• Direct numerical simulation of turbulent compression ramp flow
• Large-eddy simulation of the shock/turbulence interaction
• Efficient implementation of weighted ENO schemes
• Computational aeroacoustics beneath high speed transitional and turbulent boundary layers
• Generalized conservative approximations of split convective derivative operators
• Turbulence in supersonic boundary layers at moderate Reynolds number
• Direct numerical simulation of hypersonic turbulent boundary layers. Part 2. Effect of wall temperature
• Direct numerical simulation of transonic shock/boundary layer interaction under conditions of incipient separation
• Assessment of direct numerical simulation data of turbulent boundary layers
• The wall pressure signature of transonic shock/boundary layer interaction
• Direct numerical simulation of hypersonic turbulent boundary layers. Part 3. Effect of Mach number
• On the generation of sound by supersonic turbulent shear layers
• Analysis of wall-pressure fluctuation sources from direct numerical simulation of turbulent channel flow
• Relationship between wall pressure and velocity-field sources
• The fluctuating pressure field in a supersonic turbulent boundary layer
• Turbulent Flows
• Vortex organization in the outer region of the turbulent boundary layer
• Compressibility effects and turbulence scalings in supersonic channel flow
• A numerical study of turbulent supersonic isothermal-wall channel flow
• Compressible turbulent channel flows: DNS results and modelling
• Reynolds number effects on the Reynolds-stress budgets in turbulent channels
• Some Statistical Properties of the Pressure Field Radiated by a Turbulent Boundary Layer
• Effect of wall cooling on boundary-layer-induced pressure fluctuations at Mach 6
• Wall effects on pressure fluctuations in turbulent channel flow
• Turbulent boundary-layer noise: direct radiation at Mach number 0.5
• Direct numerical simulation of hypersonic turbulent boundary layers: effect of spatial evolution and Reynolds number
• STREAmS: A high-fidelity accelerated solver for direct numerical simulation of compressible turbulent flows

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