Partial admission effect on the performance and vibration of a supersonic impulse turbine-Reference-Cited by-同舟云学术

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Partial admission effect on the performance and vibration of a supersonic impulse turbine

Published:2018-04 Issue: Volume:145 Page:105-115
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Lee Hang Gi,Shin Ju Hyun,Choi Chang-Ho,Jeong Eunhwan,Kwon Sejin

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference28 articles.

1. Rocket Propulsion Elements;Sutton,1992

2. Modern Engineering for Design of Liquid-propellant Rocket Engines;Huzel,1992

3. Tip clearance effect on the performance of a shrouded supersonic impulse turbine;Jeong;J. Propul. Power,2008

4. Effects of Partial Admission on Performance of a Gas Turbine;Kohl,1949

Cited by 13 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. Loss characteristics and optimization method of a compressed air energy storage radial turbine with nozzle governing;Journal of Energy Storage;2024-10

2. Energy loss analysis in two-stage turbine of compressed air energy storage system: Effect of varying partial admission ratio and inlet pressure;Energy;2024-10

3. Design and Analysis of a Single-Stage Supersonic Turbine with Partial Admission;Energy;2024-09

4. CFD and Taguchi based optimization of air driven single stage partial admission axial turbine blade profiles;Energy;2024-03

5. Development of a cooling and power generation prototype integrating an axial micro-turbine in an absorption chiller;Applied Thermal Engineering;2023-09

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