Three-dimensional flow investigation of a high-pressure turbine with rotor tip desensitization based on Winglet geometry

Author:

Maia Ana A. G.ORCID,Silva Lucilene M.,Tomita Jesuíno T.,Bringhenti Cleverson

Funder

coordenação de aperfeiçoamento de pessoal de nível superior

fundação de amparo à pesquisa do estado de são paulo

conselho nacional de desenvolvimento científico e tecnológico

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,General Engineering,Aerospace Engineering,Automotive Engineering,Industrial and Manufacturing Engineering,Applied Mathematics

Reference56 articles.

1. An G, Wu Y, Lang J, Chen Z (2021) Analysis of characteristics and mechanism of flow unsteadiness in a transonic compressor. J Braz Soc Mech Sci Eng 43:98. https://doi.org/10.1007/s40430-021-02830-y

2. Maia AA, Kapat JS, Tomita JT, Silva JF, Bringhenti C, Cavalca DF (2020) Preconditioning methods for compressible flow CFD codes: revisited. Intern J Mech Sci 186:105898

3. Filho TGL, Barkett Botan AC, Villa Nova HF, Mambeli Barros R, Braga da Silva FD, Saavedra OR (2014) CFX modeling of an axial turbine with symmetrical blades and reversible flow for tidal power plants. Energy Dev 860:1823–1827

4. Silva LM, Tomita JT, Bringhenti C (2017) Numerical investigation of a Hpt with different rotor tip configurations in terms of pressure ratio and efficiency. Aerosp Sci Technol 63:33–40

5. Silva LM (2012) Cálculo do escoamento em uma turbina axial de alta pressão com diferentes configurações na geometria do topo do rotor utilizando técnicas de CFD. Cálculo do escoamento em uma turbina axial de alta pressão com diferentes configurações na geometria do topo do rotor utilizando técnicas de CFD. São José dos Campos

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