Robust airfoil optimization to achieve drag reduction over a range of Mach numbers

By Wu Li, L. Huyse, S. Padula. 2002

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Aerodynamic shape optimization for minimum robust drag and lift reliability constraint (2016, background): “The constrained optimization problem is defined as [23,46]”
CFD-based optimization of hovering rotors using radial basis functions for shape parameterization and mesh deformation (2013, methodology): “Compressible CFD has been used in numerous optimizations of two-dimensional aerofoil sections (Hicks and Henne 1978; Li et al. 2002), three-dimensional aircraft (Chung and Alonso 2004; Reuther et al.”
A benchmark of kriging-based infill criteria for noisy optimization (2013, background): “Examples of such simulators can be found in a wide range of applications, including nuclear safety assessment [9], discrete event simulation [1], acoustic wave propagation in turbulent fluids [17], airfoil optimization [23], design of composite materials [32, 31] and experimental measurements in mec”