Low speed high alpha prediction on F-16XL aircraft
2014 (English)In: 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014Article in journal (Refereed) Published
This article presents the comparisons of the results of the CFD study around the F- 16XL CAWAPI configuration. The progress since the original CAWAPI has been made on the solver side by implementing several numerical techniques improving convergence of the numerical process as well as lowering numerical viscosity needed to stabilize the calculations. In addition, innovative hybrid RANS-LES model (HYB0) has been tested and a new much denser grid has been generated.
Place, publisher, year, edition, pages
IdentifiersURN: urn:nbn:se:kth:diva-168122ScopusID: 2-s2.0-84902826849OAI: oai:DiVA.org:kth-168122DiVA: diva2:816080
QC 201506022015-06-022015-05-272015-06-02Bibliographically approved