Outline: 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.
CFD Analysis in Advance of the NASA Juncture Flow Experiment
AIAA Aviation and Aeronautics Forum (Aviation 2017) ; 2017 ; Denver, CO, United States
08.06.2017
Sonstige
Keine Angabe
Englisch
CFD Analysis in Advance of the NASA Juncture Flow Experiment (AIAA 2017-4127)
British Library Conference Proceedings | 2017
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