Turbine rim seal gas path flow ingestion mechanisms-Reference-Cited by-同舟云学术

Turbine rim seal gas path flow ingestion mechanisms

Published:1994-06-27 Issue: Volume: Page:
ISSN:
Container-title:30th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-2703

Reference29 articles.

1. Abe, T., Kikuchi, J. and Takeuchi, H. 1979, "An Investigation of Turbine Disk Cooling (Experimental Investigationand Observation of Hot Gas Flow into a Wheel Space)", 13th CIMAG Cong., Vienna, Paper No.GT30.

2. Effective Sealing of a Disk Cavity Using a Double-Toothed Rim Seal

3. Campbell, D.A.; 1978 "Gas Turbine Disc Sealing SystemDesign";AGARD-CP-237, p.18-I.

Cited by 6 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. Analysis of Ingress Into the Downstream Wheel Space of a 1.5-Stage Turbine By Full Circumference and Single Blade Passage Large-Eddy Simulations;Journal of Turbomachinery;2024-04-04

2. Steady-state analysis of purge flow passage on the performance of the high-pressure transonic axial turbine at different mass flow ratios;Sādhanā;2024-02-08

3. Performance of a Turbine Rim Seal Subject to Rotationally-Driven and Pressure-Driven Ingestion;Journal of Engineering for Gas Turbines and Power;2021-05-28

4. Effects of Purge Flow Configuration on Sealing Effectiveness in a Rotor–Stator Cavity;Journal of Engineering for Gas Turbines and Power;2018-07-12

5. Modulation and Radial Migration of Turbine Hub Cavity Modes by the Rim Seal Purge Flow;Journal of Turbomachinery;2016-09-20