Design of a high-performance centrifugal compressor impeller and an investigation on the linear effects of the hub-Reference-Cited by-同舟云学术

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Design of a high-performance centrifugal compressor impeller and an investigation on the linear effects of the hub

Published:2022-02-01 Issue:2 Volume:12 Page:025322
ISSN:2158-3226
Container-title:AIP Advances
language:en
Short-container-title:AIP Advances

Author:

Yang Xinle¹^ORCID,Tang Meiling¹,Li Song¹^ORCID,Li Weikang¹

Affiliation:

1. Liaoning Technical University, School of Mechanical Engineering, Fuxin 123000, Liaoning Province, China

Funder

Natural Science Foundation of Liaoning Province

Xingliao Yingcai Program of Liaoning Province

Liaoning Province Department of Education Project

Publisher

AIP Publishing

Subject

General Physics and Astronomy

Link

https://aip.scitation.org/doi/pdf/10.1063/5.0066151

Reference18 articles.

1. Effect of splitter leading edge location on performance of an automotive turbocharger compressor

2. Improving Centrifugal Compressor Performance by Optimizing the Design of Impellers Using Genetic Algorithm and Computational Fluid Dynamics Methods

3. Centrifugal Compressor Performance Improvements Through Impeller Splitter Location

4. Centrifugal Compressor Performance Improvement through Multi Splitter Impeller

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1. Investigating the mechanism of flow of transonic compact crossover tandem diffuser;Physics of Fluids;2024-07-01

2. Study of blade moment calculation on variable geometry turbine adjusting mechanism;Journal of Physics: Conference Series;2024-07-01

3. Review on Performance Assessment of Centrifugal Compressors;Lecture Notes in Mechanical Engineering;2024

4. Numerical Investigations and Artificial Neural Network-Based Performance Prediction of a Centrifugal Fan Having Innovative Hub Geometry Designs;Applied System Innovation;2023-11-06

5. Performance Analysis of Centrifugal Blowers with Inlet Guide Vane Control Under Different Inlet Conditions;2023 11th International Conference on ENERGY and ENVIRONMENT (CIEM);2023-10-26

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