... optimization method, requires two main building blocks: a non-linear Navier–Stokes solver to evaluate the optimized geometry, and an efficient tool to compute the gradient. Navier-Stokes equations design engineering blades gradient methods turbines 28 07 2006 31 07 2006 21 03...

..., “The Use of Be´zier Polynomial Patches to Define Geometrical Shape of the Flow Channels of Compressors,” ASME Paper 88-GT-60. Burguburu, S., Toussaint, C., and Leroy, G., 2001, “Numerical Optimization for Turbomachinery Blades Aerodynamic Design Using a Gradient Method Coupled With a Navier-Stokes...