Hybrid continuum/DSMC computation of rocket mode lightcraft flow in near space with high temperature and rarefaction effect

DOI10.1016/j.compfluid.2008.01.024zbMath1242.76186OpenAlexW2082948738MaRDI QIDQ435398

Yanji Hong, Qian Li, Zi-Niu Wu, Shan-Shu Xu

Publication date: 11 July 2012

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

Full work available at URL: https://doi.org/10.1016/j.compfluid.2008.01.024

Mathematics Subject Classification ID

Related Items (3)

Hybrid simulations of rarefied supersonic gas flows in micro-nozzles ⋮ A parallelized hybrid N-S/DSMC-IP approach based on adaptive structured/unstructured overlapping grids for hypersonic transitional flows ⋮ Development and validation of a coupled Navier-Stokes/DSMC simulation for rarefied gas flow in the production process for oleds

Cites Work

• A hybrid particle-continuum method applied to shock waves
• Direct simulation of gas flows at the molecular level

This page was built for publication: Hybrid continuum/DSMC computation of rocket mode lightcraft flow in near space with high temperature and rarefaction effect