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
2014-01-01
Sonstige
Keine Angabe
Englisch
Robust, optimal subsonic airfoil shapes
NTRS | 2008
|COMPARISON BETWEEN AERODYNAMIC AND AEROACOUSTIC PERFORMANCE OF SUBSONIC AIRFOIL SHAPES
British Library Conference Proceedings | 2012
|Unsteady thin-airfoil theory for subsonic flow.
AIAA | 1973
|