Aerothermodynamics optimal design of a multistage axial compressor in a gas turbine using directly manipulated free-form deformation
The compressor global geometric model including the endwall and the blade is parameterized read more based on a directly manipulated free-form deformation (DFFD) approach.A meridional flow streamline curvature method for solving inverse and forward problems is applied to the reverse design and performance analysis of the compressor.Combined with an