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CFD Analysis in Advance of the NASA Juncture Flow ExperimentOutline: Experiment Motivation, Goals, Model Design; Wing Candidates; Risk reduction experiments -NASA Ames Test Cell 2 (TC2) 32 inch by 48 inch, 3 percent semispan -Virginia Tech Stability Tunnel 6 foot, 2.5 percent fullspan -NASA Langley 14 by 22 Foot Subsonic Tunnel (14 by 22) 6 percent fullspan; Results from 14 by 22 6 percent risk reduction -CFD (Computational Fluid Dynamics) Free Air -CFD with 14 by 22 WT (Wind Tunnel) walls -Risk Reduction Experiment oil flow; Observations and Upcoming Experiment.
Document ID
20190025398
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Lee, Henry (Science and Technology Corp. Moffett Field, CA, United States)
Pulliam, Thomas (NASA Ames Research Center Moffett Field, CA, United States)
Neuhart, Dan (NASA Langley Research Center Hampton, VA, United States)
Kegerise, Mike (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
May 29, 2019
Publication Date
June 8, 2017
Subject Category
Fluid Mechanics And Thermodynamics
Aerodynamics
Report/Patent Number
ARC-E-DAA-TN43281-1
Meeting Information
Meeting: AIAA Aviation and Aeronautics Forum (Aviation 2017)
Location: Denver, CO
Country: United States
Start Date: June 5, 2017
End Date: June 9, 2017
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
CONTRACT_GRANT: NNA16BD60C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee

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