Three-dimensional unsteady simulation of a multistage axial compressor with labyrinth seals and its effects on overall performance and flow characteristics-Reference-Cited by-同舟云学术

Three-dimensional unsteady simulation of a multistage axial compressor with labyrinth seals and its effects on overall performance and flow characteristics

Published:2019-03 Issue: Volume:86 Page:683-693
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Kim Sangjo,Kim Kuisoon,Son Changmin

Funder

Korea Institute of Energy Technology Evaluation and Planning

Ministry of Trade, Industry and Energy

MOTIE

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference28 articles.

1. Aerodynamic performance of multi-stage axial compressor considering cold-to-hot deformation effect;Kim;Int. J. Aeronaut. Space Sci.,2018

2. Experimental Investigation of the Total Temperature Increase and Swirl Development in Rotating Labyrinth Seals;Denecke,2005

3. Impact of Rotational Speed on the Discharge Characteristic of Stepped Labyrinth Seals;Paolillo,2007

4. Experimental Investigation on Leakage Loss and Heat Transfer in a Straight Through Labyrinth Seal;Micio,2011

5. Effects of Shrouded Stator Cavity Flows on Multistage Axial Compressor Aerodynamic Performance;Wellborn,1996

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