Chemically reacting hypersonic flows over 3D cavities: flowfield structure characterisation

DOI10.1016/j.compfluid.2018.01.029zbMath1390.76909OpenAlexW2792273240MaRDI QIDQ1649688

Rodrigo C. Palharini, Craig White, Thomas J. Scanlon

Publication date: 28 June 2018

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

Full work available at URL: https://strathprints.strath.ac.uk/64271/1/Palharini_etal_CF_2018_Chemically_reacting_hypersonic_flows_over_3D_cavities.pdf

zbMATH Keywords

rarefied gasDSMCreentrycavity flowsthermal protection system

Mathematics Subject Classification ID

Rarefied gas flows, Boltzmann equation in fluid mechanics (76P05) Reaction effects in flows (76V05) Hypersonic flows (76K05)

Cites Work

• Unnamed Item
• Effects of incomplete surface accommodation on non-equilibrium heat transfer in cavity flow: a parallel DSMC study
• Reduction of simulation cost and error for particle simulations of rarefied flows
• Benchmark numerical simulations of rarefied non-reacting gas flows using an open-source DSMC code
• Statistical error analysis for the direct simulation Monte Carlo technique
• Experimental and computational study of laminar cavity flows at hypersonic speeds
• Time step truncation error in direct simulation Monte Carlo
• Analysis of discretization in the direct simulation Monte Carlo
• Numerical simulation of supersonic flow over a three-dimensional cavity
• A threshold line dissociation model for the direct simulation Monte Carlo method
• A set of model cross sections for the Monte Carlo simulation of rarefied real gases: Atom–diatom collisions

This page was built for publication: Chemically reacting hypersonic flows over 3D cavities: flowfield structure characterisation