Source Term Based Modeling of Rotating Cavitation in Turbopumps
Author:
Affiliation:
1. Rolls-Royce plc, 62 Buckingham Gate, London, SW1E 6AT, UK e-mail:
2. Assistant Professor Faculty of Aerospace Engineering, Flight Performance & Propulsion Section, Building 62, Office 7.11, Kluyverweg 1, Delft, 2629 HS, The Netherlands e-mail:
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/doi/10.1115/1.4042302/6183931/gtp_141_06_061002.pdf
Reference32 articles.
1. Hydraulic and Mechanical Performance of LE-7 LOX Pump Inducer;J. Propul. Power,1993
2. Overview of Rotating Cavitation and Cavitation Surge in the Fastrac Engine LOX Turbopump,2001
3. Ryan, R., 1994, “The Space Shuttle Main Engine Liquid Oxygen Pump High-Synchronous Vibration Issue: The Problem, The Resolution Approach, The Solution,” AIAA Paper No. 94-3153.10.2514/6.1994-3153
4. Arnone, A., Boncinelli, P., Capuani, A., Spano, E., and Rebattet, C., 2001, “‘Ariane 5’ TPLOX Inducer Design Strategies to Enhance Cavitating Performance,” Caltech Conference Repository, pp. 1–12.https://pdfs.semanticscholar.org/572f/cbfdd6602345691e04f9bab8e4dabad15091.pdf
5. Cause of Cavitation Instabilities in Three-Dimensional Inducer;Int. J. Fluid Mach. Syst.,2009
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