Improved aerodynamic design of turbomachinery bladings by numerical optimization

DOI10.1016/S1270-9638(02)00010-XzbMath1047.76587MaRDI QIDQ4462935

Arnaud le Pape, Stéphane Burguburu

Publication date: 27 May 2004

Published in: Aerospace Science and Technology (Search for Journal in Brave)

zbMATH Keywords

OptimizationBézierGradientTurbomachineryGeneticCompressor

Mathematics Subject Classification ID

Transonic flows (76H05) General theory of rotating fluids (76U05) Flow control and optimization for compressible fluids and gas dynamics (76N25)

Related Items (1)

Aerodynamic optimization of axial turbomachinery blades using parallel adaptive range differential evolution and Reynolds-averaged Navier-Stokes solutions

Uses Software

• CONMIN

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