Numerical prediction of enhanced heat flux due to shock‐on‐shock interaction in hypersonic nonequilibrium flow
DOI10.1108/09615539910255992zbMath0931.76038OpenAlexW2154715457MaRDI QIDQ4700892
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Publication date: 28 February 2000
Published in: International Journal of Numerical Methods for Heat & Fluid Flow (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1108/09615539910255992
spherecircular cylindersaerodynamic heatingconvective heat fluxadvection upstream splitting methodlower-upper symmetric Gauss-Seidel methodNavier-Stokes equation solverhypersonic thermochemical nonequilibrium air flows around blunt bodiessupersonic jet structuretwo-temperature thermochemical model of Parl
Classical flows, reactions, etc. in chemistry (92E20) Shock waves and blast waves in fluid mechanics (76L05) Finite volume methods applied to problems in fluid mechanics (76M12) Reaction effects in flows (76V05) Hypersonic flows (76K05)
Cites Work
- A new flux splitting scheme
- On the structure of an unsteady type IV interaction at Mach 8
- Implicit Schemes and LU Decompositions
- A point implicit unstructured grid solver for the euler and Navier-Stokes equations
- Numerical Computation of Two-Dimensional Viscous Blunt Body Flows with an Impinging Shock
- Application of essentially nonoscillatory schemes to unsteady hypersonic shock-shock interference heating problems
- Non-equilibrium dissociating nitrogen flow over spheres and circular cylinders
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