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.
Robust, Optimal Subsonic Airfoil Shapes
01.01.2014
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Englisch
Robust, optimal subsonic airfoil shapes
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