A new high resolution scheme for compressible viscous flows with shocks

S. Tatsumi, Luigi Martinelli, A. Jameson

Research output: Contribution to conferencePaper

10 Scopus citations

Abstract

A new flux splitting and limiting technique which yields one-point stationary shock capturing is presented. The technique is applied to the full Navier Stokes and Reynolds Averaged Navier-Stokes equations. Calculations of laminar boundary layers at subsonic and supersonic speeds are presented together with calculations of transonic flows around airfoils. The results exhibit very good agreement with theoretical solutions and existing experimental data. It is found that the proposed scheme improves the resolution of viscous flows while maintaining excellent one-point shock capturing characteristics.

Original languageEnglish (US)
Pages1-15
Number of pages15
StatePublished - Jan 1 1995
Event33rd Aerospace Sciences Meeting and Exhibit, 1995 - Reno, United States
Duration: Jan 9 1995Jan 12 1995

Other

Other33rd Aerospace Sciences Meeting and Exhibit, 1995
CountryUnited States
CityReno
Period1/9/951/12/95

All Science Journal Classification (ASJC) codes

  • Space and Planetary Science
  • Aerospace Engineering

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    Tatsumi, S., Martinelli, L., & Jameson, A. (1995). A new high resolution scheme for compressible viscous flows with shocks. 1-15. Paper presented at 33rd Aerospace Sciences Meeting and Exhibit, 1995, Reno, United States.