Experimental and numerical study on cavitation performances of a turbopump with and without an inducer
The cavitation performances and its internal flows in a centrifugal turbopump with and without a three-bladed axial inducer have been studied both experimentally and numerically. A 3D steady numerical model has been applied to simulate the cavitating flow from the inlet to the outlet ducts of the tu...
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Veröffentlicht in: | Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering Journal of aerospace engineering, 2022-05, Vol.236 (6), p.1098-1111 |
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container_title | Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering |
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creator | Fu, Yanxia Xie, Jiangfeng Shen, Yang Pace, Giovanni Valentini, Dario Pasini, Angelo D’Agostino, Luca |
description | The cavitation performances and its internal flows in a centrifugal turbopump with and without a three-bladed axial inducer have been studied both experimentally and numerically. A 3D steady numerical model has been applied to simulate the cavitating flow from the inlet to the outlet ducts of the turbopump with and without an inducer by using ANSYS CFX code. In the present work, to clarify this relationship, we conducted experiments in both cold water (T = 20°C) and hot water (T = 80°C) with a focus on the development of vapor volume fraction and head degradation by gradually reducing the inlet pressure from atmospheric conditions to the minimum allowable value at a constant rate of about 3 mbar/s. The measured and predicted cavitation performances of the turbopump with and without an inducer have been compared under different operating conditions and the temperature of the operating fluid. |
doi_str_mv | 10.1177/09544100211027045 |
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A 3D steady numerical model has been applied to simulate the cavitating flow from the inlet to the outlet ducts of the turbopump with and without an inducer by using ANSYS CFX code. In the present work, to clarify this relationship, we conducted experiments in both cold water (T = 20°C) and hot water (T = 80°C) with a focus on the development of vapor volume fraction and head degradation by gradually reducing the inlet pressure from atmospheric conditions to the minimum allowable value at a constant rate of about 3 mbar/s. The measured and predicted cavitation performances of the turbopump with and without an inducer have been compared under different operating conditions and the temperature of the operating fluid.</description><identifier>ISSN: 0954-4100</identifier><identifier>EISSN: 2041-3025</identifier><identifier>DOI: 10.1177/09544100211027045</identifier><language>eng</language><publisher>London, England: SAGE Publications</publisher><subject>Cavitation ; Cold water ; Inlet pressure ; Internal flow ; Numerical models ; Three dimensional models ; Turbine pumps</subject><ispartof>Proceedings of the Institution of Mechanical Engineers. 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Part G, Journal of aerospace engineering</title><description>The cavitation performances and its internal flows in a centrifugal turbopump with and without a three-bladed axial inducer have been studied both experimentally and numerically. A 3D steady numerical model has been applied to simulate the cavitating flow from the inlet to the outlet ducts of the turbopump with and without an inducer by using ANSYS CFX code. In the present work, to clarify this relationship, we conducted experiments in both cold water (T = 20°C) and hot water (T = 80°C) with a focus on the development of vapor volume fraction and head degradation by gradually reducing the inlet pressure from atmospheric conditions to the minimum allowable value at a constant rate of about 3 mbar/s. The measured and predicted cavitation performances of the turbopump with and without an inducer have been compared under different operating conditions and the temperature of the operating fluid.</description><subject>Cavitation</subject><subject>Cold water</subject><subject>Inlet pressure</subject><subject>Internal flow</subject><subject>Numerical models</subject><subject>Three dimensional models</subject><subject>Turbine pumps</subject><issn>0954-4100</issn><issn>2041-3025</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2022</creationdate><recordtype>article</recordtype><recordid>eNp1UMlKBDEQDaLg2PoB3gKee8zay1GGcYEBL3pu0lm0h-mkzaLO35t2BA9iXepV1Xuv4AFwidES47q-Ri1nDCNEMEakRowfgQVBDJcUEX4MFvO9nAmn4CyELcrFK7oAZv05aT-M2kaxg8IqaNOYFzJPISa1h85CKd6HKOKQYSYb50dhpQ7QGShgTL53Uxon-DHE12-LGbgUM4aDVUlqfw5OjNgFffHTC_B8u35a3Zebx7uH1c2mlBSTWDaKqKpVRgiFaaWF6nWluMI1Q6xhFDPdM94KoVXfNA1lklKjWM9qJFmtWkYLcHXwnbx7SzrEbuuSt_llR6oK8RaRrCsAPrCkdyF4bbopRyD8vsOom-Ps_sSZNcuDJogX_ev6v-ALd7l2Jw</recordid><startdate>202205</startdate><enddate>202205</enddate><creator>Fu, Yanxia</creator><creator>Xie, Jiangfeng</creator><creator>Shen, Yang</creator><creator>Pace, Giovanni</creator><creator>Valentini, Dario</creator><creator>Pasini, Angelo</creator><creator>D’Agostino, Luca</creator><general>SAGE Publications</general><general>SAGE PUBLICATIONS, INC</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>F28</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope><orcidid>https://orcid.org/0000-0003-4401-8109</orcidid></search><sort><creationdate>202205</creationdate><title>Experimental and numerical study on cavitation performances of a turbopump with and without an inducer</title><author>Fu, Yanxia ; Xie, Jiangfeng ; Shen, Yang ; Pace, Giovanni ; Valentini, Dario ; Pasini, Angelo ; D’Agostino, Luca</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c312t-8d2d69dfaad136eadbe6d5d1740484314eb459aaedb88834c33fd4b470c47d943</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2022</creationdate><topic>Cavitation</topic><topic>Cold water</topic><topic>Inlet pressure</topic><topic>Internal flow</topic><topic>Numerical models</topic><topic>Three dimensional models</topic><topic>Turbine pumps</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Fu, Yanxia</creatorcontrib><creatorcontrib>Xie, Jiangfeng</creatorcontrib><creatorcontrib>Shen, Yang</creatorcontrib><creatorcontrib>Pace, Giovanni</creatorcontrib><creatorcontrib>Valentini, Dario</creatorcontrib><creatorcontrib>Pasini, Angelo</creatorcontrib><creatorcontrib>D’Agostino, Luca</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>ANTE: Abstracts in New Technology & Engineering</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Fu, Yanxia</au><au>Xie, Jiangfeng</au><au>Shen, Yang</au><au>Pace, Giovanni</au><au>Valentini, Dario</au><au>Pasini, Angelo</au><au>D’Agostino, Luca</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Experimental and numerical study on cavitation performances of a turbopump with and without an inducer</atitle><jtitle>Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering</jtitle><date>2022-05</date><risdate>2022</risdate><volume>236</volume><issue>6</issue><spage>1098</spage><epage>1111</epage><pages>1098-1111</pages><issn>0954-4100</issn><eissn>2041-3025</eissn><abstract>The cavitation performances and its internal flows in a centrifugal turbopump with and without a three-bladed axial inducer have been studied both experimentally and numerically. A 3D steady numerical model has been applied to simulate the cavitating flow from the inlet to the outlet ducts of the turbopump with and without an inducer by using ANSYS CFX code. In the present work, to clarify this relationship, we conducted experiments in both cold water (T = 20°C) and hot water (T = 80°C) with a focus on the development of vapor volume fraction and head degradation by gradually reducing the inlet pressure from atmospheric conditions to the minimum allowable value at a constant rate of about 3 mbar/s. The measured and predicted cavitation performances of the turbopump with and without an inducer have been compared under different operating conditions and the temperature of the operating fluid.</abstract><cop>London, England</cop><pub>SAGE Publications</pub><doi>10.1177/09544100211027045</doi><tpages>14</tpages><orcidid>https://orcid.org/0000-0003-4401-8109</orcidid></addata></record> |
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subjects | Cavitation Cold water Inlet pressure Internal flow Numerical models Three dimensional models Turbine pumps |
title | Experimental and numerical study on cavitation performances of a turbopump with and without an inducer |
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