PhD Thesis, Technical University of Catalonia, 2008. Neural Networks for Variational Problems in Engineering. Imperial College of Science, Technology and Medicine (London, United Kingdom), 2006. Master’s thesis, Department of Aeronautics. Technical report, NASA RP-1218, July 1989.Ī neural networks approach for aerofoil noise prediction.
Scaled sound pressure level, in decibels.
Suction side displacement thickness, in meters.Ħ. Free-stream velocity, in meters per second.ĥ. The span of the airfoil and the observer position were the same in all of the experiments.Ĥ. The NASA data set comprises different size NACA 0012 airfoils at various wind tunnel speeds and angles of attack. Provide the names, email addresses, institutions, and other contact information of the donors and creators of the data set. Click here to try out the new site.ĭownload: Data Folder, Data Set DescriptionĪbstract: NASA data set, obtained from a series of aerodynamic and acoustic tests of two and three-dimensional airfoil blade sections conducted in an anechoic wind tunnel. Notable models to have S-foils were the T-65B X-wing starfighter manufactured. The foils were locked in the closed position in normal flight, but when engaged in combat the foils spread open into an attack position. Check out the beta version of the new UCI Machine Learning Repository we are currently testing! Contact us if you have any issues, questions, or concerns. S-foils, also known as Strike foils, were movable wings attached to the X-wing starfighter, the ARC-170 starfighter, and the Outland TIE fighter, sometimes equipped with weaponry.
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