Construction and application research of HLL-HLLC scheme

Lin Fu, Zheng Hong Gao, Xiao Dong Zhang

Research output: Contribution to journalArticlepeer-review

6 Scopus citations

Abstract

HLLC is one kind of schemes which resolve shock, contact, and rarefaction waves exactly and has high value of application in compressible fluid simulation. HLL scheme cannot deal with the contact and shear waves accurately, thus it has much more dissipation compared with the HLLC scheme. However, numerical tests have illustrated that HLLC scheme may suffer from shock instability phenomena in the vicinity of strong shock waves while it performs well in low speed and subsonic flow. HLL-HLLC scheme which is suitable for a larger range of flow is proposed through mathematical analyses of HLLC and HLL scheme. The new proposed scheme indicates the property of HLLC which has low order dissipation in low speed flow and can overcome the shortcoming of shock instability phenomena in high speed flow. The effectiveness and robustness of the proposed scheme free from shock instability phenomena is demonstrated through three numerical simulations: hypersonic flow on double wedge configuration, supersonic flow over backward-facing step and hypersonic flow over blunt body.

Original languageEnglish
Pages (from-to)116-122+135
JournalKongqi Donglixue Xuebao/Acta Aerodynamica Sinica
Volume32
Issue number1
DOIs
StatePublished - Feb 2014

Keywords

  • Compressible flow
  • High resolution method
  • HLL
  • HLLC
  • Shock instability

Fingerprint

Dive into the research topics of 'Construction and application research of HLL-HLLC scheme'. Together they form a unique fingerprint.

Cite this