Robust airfoil optimization to achieve consistent drag reduction over a mach range
By: Wu Li, Luc Huyse, Sharon Padula.
Contributors: Huyse, Luc.; Padula, Sharon.; Langley Research Center.
Series: ICASE report -- no. 2001-22.; [NASA contractor report] -- NASA/CR-2001-211042.; NASA contractor report -- NASA CR-211042.
Publisher: National Aeronautics and Space Administration, Langley Research Center; Available from NASA Center for AeroSpace Information
Published: 2001
Place of publication: Hampton, Va; Hanover, MD
Language: eng
Format: Microform
Subjects: Drag reduction.; Airfoils.; Aerodynamic drag.; Mach number.; Optimization.; Robustness (Mathematics).
Notes: Shipping list no.: 2002-0546-M.

Also available via Internet from the NASA web site. Address as of 2/26/04: http://techreports.larc.nasa.gov/icase/2001/icase-2001-22.pdf; current access available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2001] 1 microfiche.