Reynolds-Stress Model Computations of NASA Juncture Flow Experiment
Author:
Affiliation:
1. DLR Braunschweig, Lilienthalplatz 7, D-38108 Braunschweig, Germany
2. NASA Langley Research Center, MS 128, Hampton 23681, Virginia
Funder
NASA Transformational Tools and Technologies Project
German national air transport research program Lufo V
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060510
Reference39 articles.
1. DurbinP. A.Pettersson ReifB. A., Statistical Theory and Modeling for Turbulent Flows, Wiley, Chichester, England, Reprint, 2003.
2. Turbulent Secondary Flows
3. Abridged Summary of the Third AIAA Computational Fluid Dynamics Drag Prediction Workshop
4. Summary of Data from the Fifth Computational Fluid Dynamics Drag Prediction Workshop
5. RumseyC. L.NeuhartD. H.KegeriseM. A. “The NASA Juncture Flow Experiment: Goals, Progress, and Preliminary Testing (Invited),” AIAA Paper 2016-1557, 2016. 10.2514/6.2016-1557
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