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 based on a directly manipulated free-form deformation (DFFD) approach.A meridional flow streamline curvature method for solving inverse and forward problems Tools is applied to the reverse design and performance analysis of the compressor.Combined with an imp