Experimental testing for the influences of rotation and tip clearance on the labyrinth seal in a compressor stator well-Reference-Cited by-同舟云学术

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Experimental testing for the influences of rotation and tip clearance on the labyrinth seal in a compressor stator well

Published:2017-12 Issue: Volume:71 Page:556-567
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Kong Xiaozhi,Liu Gaowen,Liu Yuxin,Zheng Longxi

Funder

Shenyang Engine Design & Research Institute

AVIC Commercial Aircraft Engine Co. LTD

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference21 articles.

1. Numerical Study on the Effect of Geometrical Parameters on the Labyrinth-Honeycomb Seal Performance;Alizadeh,2014

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

3. Numerical and Experimental Investigation of Sealing Characteristics on Typical Labyrinth Seals in Aeroengine;Ji,2008

4. Incompressible Flow in Stepped Labyrinth Seals;Chi,1985

5. Determining and Improving Labyrinth Seal Performance in Current and Advanced High Performance Gas Turbines;Stocker,1978

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