Inverse design is an important part of the initial design stage of blade profile, while the
traditional inverse design methods are highly dependent on design experience and physical …

An iterative procedure for three-dimensional blade design is presented, in which the three-
dimensional blade shape is modified using a physical algorithm, based on the transpiration …

An adjoint-based shape optimization approach for supersonic turbine cascades is proposed
for application to organic Rankine cycle (ORC) turbines. The algorithm is based on an …

The wakes behind turbine blade trailing edges are characterized by large-scale periodic
vortex patterns known as the von Karman vortex street. The failure of steady-state Navier …

This paper presents a novel iterative viscous inverse design method for turbomachinery
blading. It is made up of two steps: the first one consists of an analysis by means of a Navier …

This work proposes an automated strategy for the preliminary design of turbomachinery,
based on the application of a throughflow code and of a highly flexible and efficient …

A two-dimensional viscous inverse method for the design of compressor and turbine blades
is presented. It iteratively modifies an initial geometry until a prescribed pressure distribution …

AERODYNAMIC analysis of the flow in the blade row passages of modern gas turbine
engines is routinely performed using computational fluid dynamics (CFD). However …

To further improve the efficiency of turbomachinery, an advanced aerodynamic optimization
system has been developed for the turbomachinery blade optimization design. The system …

An adjoint-based shape optimization approach for supersonic turbine cascade is proposed.
The algorithm is based on a discrete adjoint method, state-of-the-art parametrization …