A theoretical model for ingress through turbine rim seals based on physically-observed unsteadiness-Reference-Cited by-同舟云学术

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A theoretical model for ingress through turbine rim seals based on physically-observed unsteadiness

Published:2024-04 Issue: Volume:106 Page:109300
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:

Tang Hui^ORCID,Scobie James A.,Wang Zheng,Lock Gary D.

Publisher

Elsevier BV

Reference28 articles.

1. Prediction of flows in enclosed rotor–stator cavities;Bailey;Phys. Fluids,2022

2. Unsteady flow phenomena in turbine rim seals;Beard;ASME. J. Eng. Gas Turbines Power,2017

3. Performance of a turbine rim seal subject to rotationally-driven and pressure-driven ingestion;Bru Revert;ASME. J. Eng. Gas Turbines Power,2021

4. Interaction of rim seal and annulus flows in an axial flow turbine;Cao;ASME. J. Eng. Gas Turbines Power,2004

5. Rim sealing of rotor-stator wheelspaces in the presence of external flow;Chew,1994

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Evolution mechanism and parametric investigation of relative negative pressure zone in spiral groove gas face seal for aero-engine at high rotational speed;International Journal of Heat and Fluid Flow;2024-07

2. Ingress Wave Model with Purge-Mainstream Density Ratio;2024

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