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Low speed high alpha prediction on F-16XL aircraft
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering, Aerodynamics.
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering, Aerodynamics.
Swedish Defernce Research Agency, FOI, Stockholm, Sweden .
2014 (English)In: 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014, American Institute of Aeronautics and Astronautics, 2014Conference paper, Published paper (Refereed)
Abstract [en]

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
American Institute of Aeronautics and Astronautics, 2014.
Keyword [en]
F-16XL aircraft, Hybrid RANS-LES, Low speed, Numerical process, Numerical techniques, Numerical viscosity
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:kth:diva-168122Scopus ID: 2-s2.0-84902826849ISBN: 978-162410256-1 (print)OAI: oai:DiVA.org:kth-168122DiVA: diva2:816080
Conference
52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014, National Harbor, MD, United States, 13 January 2014 through 17 January 2014
Note

QC 20150602

Available from: 2015-06-02 Created: 2015-05-27 Last updated: 2017-01-16Bibliographically approved

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Output format
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