Robust airfoil optimization to achieve consistent drag reduction over a mach range
An edition of Robust airfoil optimization to achieve consistent drag reduction over a mach range (2001)
By Wu Li
Publish Date
2001
Publisher
National Aeronautics and Space Administration, Langley Research Center,Available from NASA Center for AeroSpace Information
Language
eng
Pages
-
1-2 of 2 Editions
Robust airfoil optimization to achieve consistent drag reduction over a mach range
Language: eng
Published In: 2001
Publisher: National Aeronautics and Space Administration, Langley Research Center, Available from NASA Center for AeroSpace Information
Robust airfoil optimization to achieve consistent drag reduction over a mach range
Language: eng
Published In: 2001
Publisher: National Aeronautics and Space Administration, Langley Research Center, Available from NASA Center for AeroSpace Information