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Synthesis of Hybrid Computational Fluid Dynamics Results for F-16XL Aircraft Aerodynamics
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2017 (English)In: Journal of Aircraft, ISSN 0021-8669, E-ISSN 1533-3868, Vol. 54, no 6, p. 2100-2114Article in journal (Refereed) Published
Abstract [en]

A synthesis is presented of recent numerical predictions for the F-16XL aircraft flowfields and aerodynamics. The computational analyses were all performed with hybrid Reynolds-averaged Navier-Stokes/large-eddy simulation formulations, with an emphasis on unsteady flows and associated aerodynamics, and results from five computational methods are included. The work focused on one particular low-speed high angle-of-attack flight-test condition, and comparisons against flight-test data are included. This work represents the third coordinated effort using the F-16XL aircraft, and a unique flight-test dataset, to advance the knowledge of slender airframe aerodynamics as well as the capability for predicting these aerodynamics with advanced computational fluid dynamics formulations. The prior efforts were identified as the Cranked-Arrow Wing Aerodynamics Project International.

Place, publisher, year, edition, pages
2017. Vol. 54, no 6, p. 2100-2114
National Category
Vehicle Engineering
Identifiers
URN: urn:nbn:se:kth:diva-220285DOI: 10.2514/1.C034053ISI: 000416574600007Scopus ID: 2-s2.0-85036608267OAI: oai:DiVA.org:kth-220285DiVA, id: diva2:1169100
Note

QC 20171222

Available from: 2017-12-22 Created: 2017-12-22 Last updated: 2017-12-22Bibliographically approved

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Rizzi, Arthur

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