Experimental test of a 3D parameterized vane cascade with non-axisymmetric endwall
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference25 articles.
1. Optimization and knowledge discovery of a three-dimensional parameterized vane with nonaxisymmetric endwall;Song;J. Propuls. Power,2018
2. A nonaxisymmetric endwall design approach and its computational assessment in the NGV of an HP turbine stage;Özhan;Aerosp. Sci. Technol.,2015
3. Turbine blade row optimization through endwall contouring by an adjoint method;Luo;J. Propuls. Power,2015
4. Endwall Secondary Flow Control in a High Speed Compressor Cascade with Vortex Generator Jets;Liu,2016
5. Non-Axisymmetric Endwall Profiling in the HP NGVs of an Axial Flow Gas Turbine;Rose,1994
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