Investigation of aerodynamic effects and dominant design variables of cavity squealer-tip in three-dimensional performance of a centrifugal compressor-Reference-Cited by-同舟云学术

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Investigation of aerodynamic effects and dominant design variables of cavity squealer-tip in three-dimensional performance of a centrifugal compressor

Published:2024-09 Issue: Volume:152 Page:109382
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Heidarian Shahri Mojtaba,Habibzadeh Saeid,Madadi Ali^ORCID,Benini Ernesto

Publisher

Elsevier BV

Reference24 articles.

1. On the aerodynamics of swept and leaned transonic compressor rotors;Benini;ASME Turbo Expo.,2006

2. Three-dimensional multi-objective design optimization of a transonic compressor rotor;Benini;J. Propul. Power,2004

3. Three-dimensional optimization of blade lean and sweep for an axial compressor to improve the engine performance;Heidarian Shahri;J. Appl. Fluid Mech.,2023

4. A study on lean, sweep and chord length effects on aerodynamic performance of axial fan of a high-bypass ratio turbofan engine;Sarabchi;Iran. Aerospace Soc.,2021

5. Aerothermal effect of cavity welding beads on a transonic squealer tip;Vieira;J. Turbomach.,2021

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