Reynolds number effects identified with CFD methods compared to semi-empirical methods
2006 (English)In: ICAS-Secretariat - 25th Congress of the International Council of the Aeronautical Sciences 2006, Curran Associates, Inc., 2006, Vol. 3, 1566-1579 p.Conference paper (Refereed)
In order to estimate Reynolds number effects on a transonic transport aircraft CFD calculations have been performed. The CFD calculations have been done solving the RANS equations on an unstructured grid for varying Reynolds number at transonic conditions. Low Reynolds number data have been extrapolated to a higher Reynolds number condition with different scaling methodologies in order to evaluate each methods strengths and weaknesses.
Place, publisher, year, edition, pages
Curran Associates, Inc., 2006. Vol. 3, 1566-1579 p.
Aeronautics, CFD, Corrections, Reynolds number, Scaling
IdentifiersURN: urn:nbn:se:kth:diva-6183ScopusID: 2-s2.0-84896998317OAI: oai:DiVA.org:kth-6183DiVA: diva2:10821
25th Congress of the International Council of the Aeronautical Sciences 2006, Hamburg, Germany, 3 September 2006 through 8 September 2006
QC 201009032006-10-032006-10-032015-04-14Bibliographically approved