Evolution mechanism and parametric investigation of relative negative pressure zone in spiral groove gas face seal for aero-engine at high rotational speed-Reference-Cited by-同舟云学术

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Evolution mechanism and parametric investigation of relative negative pressure zone in spiral groove gas face seal for aero-engine at high rotational speed

Published:2024-07 Issue: Volume:107 Page:109362
ISSN:0142-727X
Container-title:International Journal of Heat and Fluid Flow
language:en
Short-container-title:International Journal of Heat and Fluid Flow

Author:

Li Hui,Li Guoqing,Liu Hao,Li Ang,Lu Xingen

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference30 articles.

1. Influence of fluid flow regime on performances of non-contacting liquid face seals[J];Brunetiere;ASME J. Tribol.,2002

2. Simulation of flow and heat transfer in the tip region of a brush seal[J];Chew;Int. J. Heat Fluid Flow,2004

3. Research on the performance of supercritical CO2 dry gas seal with different deep spiral groove[J];Du;J. Therm. Sci.,2019

4. Effects of grooved ring rotation and working fluid on the performance of dry gas seal[J];Du;Int. J. Heat Mass Transf.,2018

5. Research on the performance of supercritical CO2 dry gas seal with different deep spiral groove [J];Du;J. Therm. Sci.,2019

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1. A model of contact deep groove seals based on partition model and JFO boundary condition;Tribology International;2024-12

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