Numerical insights into the solution of transonic flow test cases using the Wilcox k - ω, EASM and SST models

K. A. Goodheart, S. Dykas, G. H. Schnerr

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

2 Scopus citations

Abstract

This paper demonstrates how compressibility correlations improve the numerical solution of the Wilcox k-ω model for a 2-d flow with shock, separation, and reattachment but then other test cases will be examined to see if an improvement still holds true. The SST and EASM models also have ways of handling complex flows and will be tested and compared. Of the three correlations, the Sarkar correlation shows the best agreement with experiment because it allows the closure coefficient β to go above its fully turbulent value of 0.09, which reduces k and allows the separation region to increase. A new technique, called 3-term, is used to calculate the turbulent production. This technique shows much improvement over a central difference scheme because it uses three points to approximate the derivative, which is important for the calculation of production in separated flows.

Original languageEnglish
Title of host publication41st Aerospace Sciences Meeting and Exhibit
StatePublished - 2003
Event41st Aerospace Sciences Meeting and Exhibit 2003 - Reno, NV, United States
Duration: 6 Jan 20039 Jan 2003

Publication series

Name41st Aerospace Sciences Meeting and Exhibit

Conference

Conference41st Aerospace Sciences Meeting and Exhibit 2003
Country/TerritoryUnited States
CityReno, NV
Period6/01/039/01/03

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