Robust airfoil optimization to achieve consistent drag reduction over a mach range /

Bibliographic Details
Main Author:	Li, Wu
Corporate Author:	Langley Research Center
Other Authors:	Huyse, Luc, Padula, Sharon
Format:	Government Document Book
Language:	English
Published:	Hampton, Va. : Hanover, MD : National Aeronautics and Space Administration, Langley Research Center ; Available from NASA Center for AeroSpace Information, [2001]
Series:	ICASE report ; no. 2001-22. NASA contractor report ; NASA CR-211042.
Subjects:	Drag reduction. Airfoils. Aerodynamic drag. Mach number. Optimization. Robustness (mathematics)
Online Access:	https://purl.fdlp.gov/GPO/LPS38993

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