NASA Juncture Flow Computational Fluid Dynamics Validation Experiment
Author:
Affiliation:
1. Boeing Commercial Airplanes, Seattle, Washington 98124
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061600
Reference40 articles.
1. Summary of the Fourth AIAA Computational Fluid Dynamics Drag Prediction Workshop
2. Overview and Summary of the Third AIAA High Lift Prediction Workshop
3. KegeriseM. A.NeuhartD. H. “An Experimental Investigation of a Wing-Fuselage Junction Model in the NASA Langley 14- by 22-Foot Subsonic Tunnel,” NASA TM-2019-220286, June 2019, https://ntrs.nasa.gov/citations/20190027403.
4. KegeriseM. A.NeuhartD. H.HannonJ. A.RumseyC. L. “An Experimental Investigation of a Wing-Fuselage Junction Model in the NASA Langley 14- by 22-Foot Subsonic Wind Tunnel,” AIAA Paper 2019-0077, Jan. 2019. 10.2514/6.2019-0077
5. RumseyC. L.NeuhartD. H.KegeriseM. A. “The NASA Juncture Flow Experiment: Goals, Progress, and Preliminary Testing,” AIAA Paper 2016-1557, Jan. 2016. 10.2514/6.2016-1557
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