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Shan Liu

6 papers hereh-index 6121 citations32 works total

Matching runs newest-first, so older work may not be attached to this profile yet.

author position
  • first author1
  • middle author4
  • last author1

Across the 6 of 6 papers where every author was matched, so the position is known.

fields
  • physics.flu-dyn4
  • physics.comp-ph2
same name
  • Shan Liu — 27 papers, h 34
  • Shan Liu — 9 papers, h 5
  • Shan Liu — 6 papers
  • Shan Liu — 5 papers, h 18
  • Shan Liu — 4 papers, h 1
  • Shan Liu — 4 papers, h 4

Either other researchers who publish under this name, or the same person where the external sources have not merged their records.

identity via Semantic Scholar / OpenAlex

activity
20232026
collaborators
Showing physics.flu-dynShow all

4 papers · 1 filter

physics.flu-dyn2026

Phenomenological energy exchange of diatomic gases: Comparison of Pullin and Borgnakke-Larsen models in direct simulation Monte Carlo method

Hao Jin, Sha Liu, Ningchao Ding +4

In hypersonic rarefied flows, insufficient intermolecular collisions cause significant deviations between translational and rotational temperatures, leading to strong thermal noneq…

physics.flu-dyn2025

A simplified unified wave-particle method for diatomic gases with rotational and vibrational non-equilibrium

Sirui Yang, Chengwen Zhong, Ningchao Ding +4

The hypersonic flow around near-space vehicles constitutes a multi-scale flow problem. Due to insufficient molecular collisions to achieve equilibrium, rarefied gas effects are pre…

physics.flu-dyn2024

Simplified unified wave-particle method for diatomic gases based on Rykov model

Sirui Yang, Sha Liu, Junzhe Cao +1

During the past decades, the numerical methods based on Navier-Stokes (N-S) equations and direct simulation Monte Carlo (DSMC) methods have been proved effective in simulating flow…

physics.flu-dyn2023

Hypersonic wave wall flow based on gas kinetic method

Yining Yang, Rui Zhang, Jianfeng Chen +4

The transition of hypersonic boundary layer can lead to a several-fold increase in surface heat flux and skin friction for the aircraft, significantly impacting its flight performa…

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