A technique for integrating two-dimensional Euler equations
From MaRDI portal
Publication:1088551
DOI10.1016/0045-7930(87)90005-3zbMath0612.76083OpenAlexW1971864943MaRDI QIDQ1088551
Publication date: 1987
Published in: Computers and Fluids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/0045-7930(87)90005-3
lambda-schememethod of shock-fittingquasi-one-dimensional problemstwo-dimensional, compressible, inviscid, unsteady flows
Shock waves and blast waves in fluid mechanics (76L05) Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10) Basic methods in fluid mechanics (76M99)
Related Items
Three-dimensional flow computations with shock fitting ⋮ On high-order shock-fitting and front-tracking schemes for numerical simulation of shock-disturbance interactions ⋮ Fast numerical solver for transonic flows ⋮ A tractable prescription for large-scale free flight expansion of wavefunctions ⋮ Fast moving sub-subsonic shocks in closed-end tubes ⋮ The inviscid transonic flow about a cylinder ⋮ A fast Euler solver for the solution of three‐dimensional rotational compressible flows ⋮ Numerical simulation of shock/boundary-layer interaction using an unstructured shock-fitting technique ⋮ A characteristic-type formulation of the Navier-Stokes equations for high-order upwind schemes ⋮ Completely conservative and oscillationless semi-Lagrangian schemes for advection transportation ⋮ Computations of viscous flows using a multigrid finite volume lambda formulation ⋮ Thirty-six years of shock fitting. ⋮ A front tracking method on unstructured grids.
Cites Work
- On two upwind finite-difference schemes for hyperbolic equations in non- conservative form
- The \(\lambda\)-scheme
- Comparison of different integration schemes based on the concept of characteristics as applied to the ablated blunt body problem
- A New and Improved Computational Technique for Two-Dimensional, Unsteady, Compressible Flows
- The numerical solution of hyperbolic systems of partial differential equations in three independent variables
- Numerical experiments on the leading-edge flowfield
- Upwind Second-Order Difference Schemes and Applications in Aerodynamic Flows