Direct numerical simulation of hypersonic turbulent boundary layers. Part 2. Effect of wall temperature

DOI10.1017/S0022112010000959zbMath1197.76078OpenAlexW2000760443MaRDI QIDQ3053560

No author found.

Publication date: 29 October 2010

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

Full work available at URL: https://doi.org/10.1017/s0022112010000959

Mathematics Subject Classification ID

Direct numerical and large eddy simulation of turbulence (76F65) Turbulent boundary layers (76F40) Hypersonic flows (76K05)

Related Items (47)

Effects of dimensional wall temperature on Reynolds stress budgets in a supersonic turbulent channel flow with thermally perfect gas ⋮ Predictive models for near-wall velocity and temperature fluctuations in supersonic wall-bounded turbulence ⋮ Artificial-neural-network-based nonlinear algebraic models for large-eddy simulation of compressible wall-bounded turbulence ⋮ Direct numerical simulation of hypersonic turbulent boundary layers. Part 4. Effect of high enthalpy ⋮ Turbulence in supersonic boundary layers at moderate Reynolds number ⋮ A unified temperature transformation for high-Mach-number flows above adiabatic and isothermal walls ⋮ Resolution effects in compressible, turbulent boundary layer simulations ⋮ Prediction of compressible turbulent boundary layer via a symmetry-based length model ⋮ Skin-friction and heat-transfer decompositions in hypersonic transitional and turbulent boundary layers ⋮ Thermochemical non-equilibrium effects in turbulent hypersonic boundary layers ⋮ Large-eddy simulation of a spatially-evolving supersonic turbulent boundary layer at \(M_{\infty} = 2\) ⋮ Wall-cooling effects on pressure fluctuations in compressible turbulent boundary layers from subsonic to hypersonic regimes ⋮ HTR solver: an open-source exascale-oriented task-based multi-GPU high-order code for hypersonic aerothermodynamics ⋮ Linear response analysis of supersonic turbulent channel flows with a large parameter space ⋮ Study of the linear models in estimating coherent velocity and temperature structures for compressible turbulent channel flows ⋮ Scaling and modelling of turbulence in variable property channel flows ⋮ 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 ⋮ Compressibility effects in supersonic and hypersonic turbulent boundary layers subject to wall disturbances ⋮ Reynolds number and wall cooling effects on correlations between the thermodynamic variables in hypersonic turbulent boundary layers ⋮ Linear-model-based study of the coupling between velocity and temperature fields in compressible turbulent channel flows ⋮ Effect of bulk viscosity on the hypersonic compressible turbulent boundary layer ⋮ Natural grid stretching for DNS of compressible wall-bounded flows ⋮ The influence of near-wall density and viscosity gradients on turbulence in channel flows ⋮ A new wall function method for hypersonic laminar boundary layers ⋮ Direct numerical simulations of supersonic turbulent channel flows of dense gases ⋮ Effect of wall cooling on boundary-layer-induced pressure fluctuations at Mach 6 ⋮ Reynolds analogy factor in self-similar compressible turbulent boundary layers with pressure gradients ⋮ Shock-induced heating and transition to turbulence in a hypersonic boundary layer ⋮ Investigation of species-mass diffusion in binary-species boundary layers at high pressure using direct numerical simulations ⋮ Wall Temperature Effects on the Reynold Stress of Flat-Plate Turbulent Boundary Layer: a Numerical Investigation ⋮ Linear instability of Poiseuille flows with highly non-ideal fluids ⋮ High-speed boundary-layer transition induced by a discrete roughness element ⋮ Resolvent-based study of compressibility effects on supersonic turbulent boundary layers ⋮ Implicit large eddy simulation of weakly-compressible turbulent channel flow ⋮ Direct numerical simulation of a hypersonic transitional boundary layer at suborbital enthalpies ⋮ Eulerian–Lagrangian direct numerical simulation of preferential accumulation of inertial particles in a compressible turbulent boundary layer ⋮ Effect of Mach number and plate thickness on the flow field and heat transfer characteristics of supersonic turbulent flow over a flat plate at different thermal boundary conditions ⋮ Optimal heat flux for delaying transition to turbulence in a high-speed boundary layer ⋮ The effect of thermal boundary conditions on forced convection heat transfer to fluids at supercritical pressure ⋮ Decomposition of the mean skin-friction drag in compressible turbulent channel flows ⋮ Image-based modelling of the skin-friction coefficient in compressible boundary-layer transition ⋮ Supersonic turbulent boundary layer drag control using spanwise wall oscillation ⋮ Trapped waves in supersonic and hypersonic turbulent channel flow over porous walls ⋮ Turbulence in a heated pipe at supercritical pressure ⋮ Direct numerical simulation of hypersonic turbulent boundary layers: effect of spatial evolution and Reynolds number ⋮ Statistical properties of pressure-Hessian tensor in a turbulent channel flow

Cites Work

• Unnamed Item
• Reynolds analogies and experimental study of heat transfer in the supersonic boundary layer
• Direct simulation of turbulent supersonic boundary layers by an extended temporal approach
• Turbulent boundary-layer structure in supersonic flow
• Direct numerical simulation of hypersonic turbulent boundary layers. Part 1. Initialization and comparison with experiments
• Evidence of very long meandering features in the logarithmic region of turbulent boundary layers
• Very large-scale motion in the outer layer
• Direct numerical simulation and analysis of a spatially evolving supersonic turbulent boundary layer at M=2.25
• Assessment of inflow boundary conditions for compressible turbulent boundary layers
• Direct simulation of a turbulent boundary layer up to R_θ = 1410
• Mechanisms for generating coherent packets of hairpin vortices in channel flow
• Direct numerical simulation of a supersonic turbulent boundary layer at Mach 2.5
• Vortex organization in the outer region of the turbulent boundary layer
• Direct numerical simulation of compressible turbulent channel flow between adiabatic and isothermal walls
• A numerical study of turbulent supersonic isothermal-wall channel flow
• Compressible turbulent channel flows: DNS results and modelling
• Coherent structures in direct numerical simulation of turbulent boundary layers at Mach 3
• Large-scale motions in a supersonic turbulent boundary layer

This page was built for publication: Direct numerical simulation of hypersonic turbulent boundary layers. Part 2. Effect of wall temperature