Direct numerical simulation of the laminar-turbulent transition at hypersonic flow speeds on a supercomputer

DOI10.1134/S0965542517080061zbMath1457.76085OpenAlexW2753310155MaRDI QIDQ1683184

Peng Zhang

Publication date: 6 December 2017

Published in: Computational Mathematics and Mathematical Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s0965542517080061

zbMATH Keywords

direct numerical simulationhypersonic flowsboundary layerlaminar-turbulent transition

Mathematics Subject Classification ID

Direct numerical and large eddy simulation of turbulence (76F65) Hypersonic flows (76K05) Transition to turbulence (76F06)

Related Items (2)

Excitation and development of instability in a compressible boundary layer as obtained in high-order accurate numerical simulation without introducing artificial perturbations ⋮ Gas injection and suction effect on the instability of a supersonic boundary layer

Uses Software

• PETSc

Cites Work

• Numerical modeling of the disturbances of the separated flow in a rounded compression corner
• Approximate Riemann solvers, parameter vectors, and difference schemes
• The use of fully implicit monotone schemes to model plane internal flows
• An approach to the numerical solution of the bidimensional Navier-Stokes equations using the direct calculation method
• Numerical solution of the Navier-Stokes equations using variational iteration methods
• Efficient implementation of weighted ENO schemes
• Direct numerical simulation of disturbances generated by periodic suction-blowing in a hypersonic boundary layer
• Direct Numerical Simulation on the Receptivity, Instability, and Transition of Hypersonic Boundary Layers
• An Easily Testable Design of Programmable Logic Arrays for Multiple Faults
• GMRES: A Generalized Minimal Residual Algorithm for Solving Nonsymmetric Linear Systems
• Evolution of nonlinear processes in a hypersonic boundary layer on a sharp cone
• Transition and Stability of High-Speed Boundary Layers
• Numerical simulation of stabilization of the boundary layer on a surface with a porous coating in a supersonic separated flow

This page was built for publication: Direct numerical simulation of the laminar-turbulent transition at hypersonic flow speeds on a supercomputer