ADJOINT AERODYNAMIC DESIGN OPTIMIZATION FOR BLADES IN MULTI-STAGE TURBOMACHINES: PART II -VALIDATION AND APPLICATION
This is the second part of a two-part paper. It presents four case studies. The first case is the redesign of a transonic rotor (NASA rotor 67) at a post peak efficiency operating point. The second case is a redesign of a transonic compressor stage originally designed by DLR. The redesign is carried...
| Main Authors: | , , , , , |
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| Format: | Conference item |
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2008
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Adjoint Aerodynamic Design Optimization for Blades in Multistage Turbomachines-Part II: Validation and Application
Published 2010
Conference item