A numerical study of the viscous supersonic flow past a flat plate at large angles of incidence

DOI10.1063/1.868269zbMath0832.76056OpenAlexW2091580969MaRDI QIDQ4841849

Dimitris Drikakis, Franz Durst

Publication date: 24 July 1995

Published in: Physics of Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1063/1.868269

zbMATH Keywords

Navier-Stokes equationsimplicit relaxation scheme

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Supersonic flows (76J20)

Related Items

An implicit unfactored method for unsteady turbulent compressible flows with moving boundaries, Hybrid upwind methods for the simulation of unsteady shock-wave diffraction over a cylinder, Effects of numerical diffusion on the computation of viscous supersonic flow over a flat plate

Cites Work

• ENO schemes with subcell resolution
• Efficient solution algorithms for the Riemann problem for real gases
• Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methods
• Approximate Riemann solvers, parameter vectors, and difference schemes
• On the solution of the compressible Navier--Stokes equations using improved flux vector splitting methods
• Die Überschallströmung der angestellten, ebenen Platte
• Boundary-Layer Interaction Theory
• Viscous-inviscid interactions on axisymmetric bodies of revolution in supersonic flow
• D’Alembert’s Paradox
• Approximate and exact numerical computation of supersonic flow over an airfoil
• On the High Reynolds Number Theory of Laminar Flows
• Local solution acceleration method for the Euler and Navier-Stokes equations
• The numerical solution of the asymptotic equations of trailing edge flow
• New Method for Supersonic Boundary-Layer Separations
• The laminar separation of an incompressible fluid streaming past a smooth surface
• Laminar boundary-layer reattachment in supersonic flow
• Numerical Technique for the Triple-Deck Problem
• Numerical and asymptotic solutions for the supersonic flow near the trailing edge of a flat plate at incidence
• Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactions
• On the flow near the trailing edge of a flat plate
• Self-induced separation
• On the flow near the trailing edge of a flat plate II
• Trailing edge flows
• Trailing-edge stall
• Boundary-Layer Flow Near the Trailing Edge of a Flat Plate
• Plate-injection into a separated supersonic boundary layer
• ON LAMINAR BOUNDARY-LAYER FLOW NEAR A POSITION OF SEPARATION