Understanding of tip clearance flow structure in high speed mixed flow compressor-Reference-Cited by-同舟云学术

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Understanding of tip clearance flow structure in high speed mixed flow compressor

Published:2023-09 Issue:3 Volume:12 Page:356-379
ISSN:2212-540X
Container-title:Propulsion and Power Research
language:en
Short-container-title:Propulsion and Power Research

Author:

Kumar Hemant,Mistry Chetan S.

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Fuel Technology,Aerospace Engineering,Automotive Engineering

Reference31 articles.

1. Performance Characteristics of Mixed Flow Impeller and Vaned Diffuser with Several Modifications;King,1942

2. Design and Performance of Experimental Axial-Discharge Mixed Flow Compressor, I: Impeller Design Theory;Goldstein,1948

3. Behavior of tip leakage flow behind an axial flow compressor rotor;Inoue;ASME Journal of Engineering for Gas Turbines and Power,1986

4. Structure of tip clearance flow in an isolated axial compressor rotor;Inoue;ASME Journal of Turbomachinery,1989

5. A role of tip leakage vortex breakdown in compressor rotor aerodynamics;Furukawa;ASME Journal of Turbomachinery,1999

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