NASA NTRS · 20140002367
Robust, Optimal Subsonic Airfoil Shapes
Abstract
A method has been developed to create an airfoil robust enough to operate satisfactorily in different environments. This method determines a robust, optimal, subsonic airfoil shape, beginning with an arbitrary initial airfoil shape, and imposes the necessary constraints on the design. Also, this method is flexible and extendible to a larger class of requirements and changes in constraints imposed.
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Rai, Man Mohan. 2014-01-01. Robust, Optimal Subsonic Airfoil Shapes. https://ntrs.nasa.gov/citations/20140002367
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