An efficient numerical method for highly loaded transonic cascade flow

DOI10.1007/s10665-007-9150-xzbMath1131.76038OpenAlexW2040783208MaRDI QIDQ2476673

Yi Liu

Publication date: 12 March 2008

Published in: Journal of Engineering Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10665-007-9150-x

zbMATH Keywords

shock waveboundary layermodified implicit flux-vector-splitting solver

Mathematics Subject Classification ID

Transonic flows (76H05) Finite difference methods applied to problems in fluid mechanics (76M20)

Uses Software

• FLUENT

Cites Work

• The implicit formulation of flux-vector-splitting scheme with application to transonic flows
• Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methods
• A new highly-efficient and accurate implicit flux vector splitting schemes
• Predictions of Channel and Boundary-Layer Flows with a Low-Reynolds-Number Turbulence Model
• An Implicit Factored Scheme for the Compressible Navier-Stokes Equations
• Prediction of jet flows in the supersonic nozzle and diffuser
• The analysis and modelling of dilatational terms in compressible turbulence