.... 01 10 2004 01 02 2005 aerodynamics compressors blades design engineering turbomachinery computational fluid dynamics inverse problems inverse aerodynamic shape design multistage turbomachinery CFD compressor stage matching Turbomachinery computational fluid...

... of the abscissa axis) 09 09 2003 12 01 2005 transonic flow confined flow computational fluid dynamics Navier-Stokes equations turbines blades inverse problems Mach number turbulence boundary layers Computational fluid dynamics (CFD) techniques are now sufficiently robust...

... the pitch chord ratio is fixed and no limitations are imposed on the stagger angle. When designing a new blade, for an arbitrary required pressure distribution (blind test) there is no guarantee that a solution to the inverse problem exists. The following viscous inverse design at transonic regime...