Abstract
xFLOWg -an in-house developed, three dimensional structured Navier-Stokes solver- is used in computations of NASA 65° delta wing. The case study is a part of NATO-RTA AVT-113 working group, named as Vortex Flow Experiment 2 (VFE2) [1] which investigates the vortical flow formation in order to improve the technology readiness level for military aircraft.
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References
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Tarhan, E., Ortakaya, Y., Gurdamar, E., Korkem, B. (2009). PARALLEL NAVIER-STOKES SOLUTIONS OF NASA 65° DELTA-WING. In: Parallel Computational Fluid Dynamics 2007. Lecture Notes in Computational Science and Engineering, vol 67. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-92744-0_27
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DOI: https://doi.org/10.1007/978-3-540-92744-0_27
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