An efficient CFD approach for simulating unsteady hypersonic shock-shock interference flows

DOI10.1016/S0045-7930(97)00061-3zbMath0970.76070OpenAlexW2070394521MaRDI QIDQ1974642

Hisaaki Daiguji, Shintaro Kano, Satoru Yamamoto

Publication date: 16 October 2001

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0045-7930(97)00061-3

zbMATH Keywords

Newton iterationshock-shock interferenceAUSM-based schemefourth-order accurate compact MUSCL TVD schemehigher-resolution finite difference schemesmaximum second-order accurate LU-SGS schemeunsteady hypersonic viscous flows

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Finite difference methods applied to problems in fluid mechanics (76M20) Hypersonic flows (76K05)

Related Items (1)

A multidimensional gas-kinetic BGK scheme for hypersonic viscous flow

Cites Work

• Higher-order-accurate upwind schemes for solving the compressible Euler and Navier--Stokes equations
• ENO schemes with subcell resolution
• Construction of explicit and implicit symmetric TVD schemes and their applications
• Efficient implementation of essentially nonoscillatory shock-capturing schemes. II
• A new flux splitting scheme
• A point implicit unstructured grid solver for the euler and Navier-Stokes equations
• Application of essentially nonoscillatory schemes to unsteady hypersonic shock-shock interference heating problems

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