Effect of Tip Clearance on the Cavitation Performance of a Turbopump Inducer-Reference-Cited by-同舟云学术

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Effect of Tip Clearance on the Cavitation Performance of a Turbopump Inducer

Published:2006-01 Issue:1 Volume:22 Page:174-179
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Hong Soon-Sam¹,Kim Jin-Sun¹,Choi Chang-Ho¹,Kim Jinhan¹

Affiliation:

1. Korea Aerospace Research Institute, Daejeon 305-333, Republic of Korea

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.11982

Reference11 articles.

1. Experimental Study on Rotating Cavitation of Rocket Propellant Pump Inducers

2. Observations of Oscillating Cavitation of an Inducer

3. Effects of Alternate Leading Edge Cutback on Unsteady Cavitation in 4-Bladed Inducers

4. Improvement of Inlet Flow Characteristics of LE-7A Liquid Hydrogen Pump

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1. Experimental study on the cavitation phenomenon effect on the efficiency of a turbulent premixed flame kerosene/air;Experimental Thermal and Fluid Science;2024-05

2. Design and Numerical Analysis of a High Head Inducer for a Rocket Pump;Lecture Notes in Mechanical Engineering;2024

3. Maximizing the performance of pump inducers using CFD-based multi-objective optimization;Structural and Multidisciplinary Optimization;2021-12-18

4. Research on Visualization of Inducer Cavitation of High-Speed Centrifugal Pump in Low Flow Conditions;Journal of Marine Science and Engineering;2021-11-08

5. Experimental investigation of cavitation instabilities in inducer with different tip clearances;Chinese Journal of Aeronautics;2021-09

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