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Sensitivity to physical and numerical modeling in Navier-Stokes simulations
KTH, Superseded Departments, Aeronautical and Vehicle Engineering.
2000 (English)In: Journal of Aerospace Engineering, ISSN 0893-1321, E-ISSN 1943-5525, Vol. 13, no 2, 47-51 p.Article in journal (Refereed) Published
Abstract [en]

Navier-Stokes Multiblock code solves the fully coupled system of equations simultaneously using a cell-centered finite-volume approach. This note assesses the sensitivity to some turbulence models and numerical schemes implemented in Navier-Stokes Multiblock when computing two test cases in standard mode, i.e., without tuning the code to these two cases. The cases are (1) subsonic flow around the MS(1)-0313 airfoil, and (2) transonic flow around the ONERA M6 wing, using various combinations of models (algebraic Baldwin-Lomax or Granville, one-equation Spalart-Allmaras, or the two-equation k - epsilon model of Chien) together with a numerical scheme of either the second-order central or third-order Roe upwind type.

Place, publisher, year, edition, pages
2000. Vol. 13, no 2, 47-51 p.
Keyword [en]
flow
Identifiers
URN: urn:nbn:se:kth:diva-19648ISI: 000086105300002OAI: oai:DiVA.org:kth-19648DiVA: diva2:338340
Note
QC 20100525Available from: 2010-08-10 Created: 2010-08-10 Last updated: 2017-12-12Bibliographically approved

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