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

By L. Wu, H. Luc, Padula Sharon. 2001

50 citations recorded by the source corpus.

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

Airfoil Optimization Using Practical Aerodynamic Design Requirements (2010, methodology): “[5] have used multipoint optimization techniques applied to airfoil design to achieve constant drag over a range of cruise Mach numbers.”