Numerical Analysis of Sloshing and Wave Breaking in a Small Vessel by CIP-LSM

For the prediction of sloshing in the propellant tank of a rocket vehicle, the preliminary investigation was conducted. The flow field in the propellant tank during the ballistic flight of the vehicle was experimentally reproduced with the sub-scale model. The lateral acceleration as large as about...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Veröffentlicht in:	JSME International Journal Series B Fluids and Thermal Engineering 2004, Vol.47(4), pp.709-715
Hauptverfasser:	HIMENO, Takehiro, WATANABE, Toshinori, NONAKA, Satoshi, NARUO, Yoshihiro, INATANI, Yoshifumi
Format:	Artikel
Sprache:	eng
Schlagworte:	CIP Level Set MARS Propellant Management Sloshing Wave Breaking
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

container_end_page	715
container_issue	4
container_start_page	709
container_title	JSME International Journal Series B Fluids and Thermal Engineering
container_volume	47
creator	HIMENO, Takehiro WATANABE, Toshinori NONAKA, Satoshi NARUO, Yoshihiro INATANI, Yoshifumi
description	For the prediction of sloshing in the propellant tank of a rocket vehicle, the preliminary investigation was conducted. The flow field in the propellant tank during the ballistic flight of the vehicle was experimentally reproduced with the sub-scale model. The lateral acceleration as large as about 0.8G was provided with a mechanical exciter and the deformation of the liquid surface in the small vessel was visualized with a high-speed camera. The sloshing phenomena were also simulated with the CFD code, called CIP-LSM. The important features of surface deformation and wave breaking were successfully reproduced in the computation.
doi_str_mv	10.1299/jsmeb.47.709
format	Article
fullrecord	<record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_29409602</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>29409602</sourcerecordid><originalsourceid>FETCH-LOGICAL-c582t-2da759dbf561efe8c69748f6179943bdc2285b4b82ffddeac40e0fe14b5500cf3</originalsourceid><addsrcrecordid>eNpd0FtLwzAUB_AiCs7pmx8gIPhkZ5ImTfM4h5fBvMC8PIY0Pdk603YmnbBvb7fJBF9yQvI7B84_is4JHhAq5fUiVJAPmBgILA-iHkmYiHkiyOH2juMMc3YcnYSwwDhJeCp70ePTqgJfGu3QsNZuHcqAGoumrgnzsp4hXRfoQ38DuvGgPzcvZY00mlbaOfQOIYBD-RqNxi_xZPp4Gh1Z7QKc_dZ-9HZ3-zp6iCfP9-PRcBIbntE2poUWXBa55SkBC5lJpWCZTYmQkiV5YSjNeM7yjFpbFKANw4AtEJZzjrGxST-63M1d-uZrBaFVVRkMOKdraFZBUcmwTDHt4MU_uGhWvls0KMJSwWmapBt1tVPGNyF4sGrpy0r7tSJYbZJV22QVE6pLtuPDHV-EVs9gj7VvS-PgD7Pd0fXs_8xcewV18gN5nIMZ</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>1467526362</pqid></control><display><type>article</type><title>Numerical Analysis of Sloshing and Wave Breaking in a Small Vessel by CIP-LSM</title><source>J-STAGE (Japan Science & Technology Information Aggregator, Electronic) Freely Available Titles - Japanese</source><source>Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals</source><creator>HIMENO, Takehiro ; WATANABE, Toshinori ; NONAKA, Satoshi ; NARUO, Yoshihiro ; INATANI, Yoshifumi</creator><creatorcontrib>HIMENO, Takehiro ; WATANABE, Toshinori ; NONAKA, Satoshi ; NARUO, Yoshihiro ; INATANI, Yoshifumi</creatorcontrib><description>For the prediction of sloshing in the propellant tank of a rocket vehicle, the preliminary investigation was conducted. The flow field in the propellant tank during the ballistic flight of the vehicle was experimentally reproduced with the sub-scale model. The lateral acceleration as large as about 0.8G was provided with a mechanical exciter and the deformation of the liquid surface in the small vessel was visualized with a high-speed camera. The sloshing phenomena were also simulated with the CFD code, called CIP-LSM. The important features of surface deformation and wave breaking were successfully reproduced in the computation.</description><identifier>ISSN: 1340-8054</identifier><identifier>EISSN: 1347-5371</identifier><identifier>DOI: 10.1299/jsmeb.47.709</identifier><language>eng</language><publisher>Tokyo: The Japan Society of Mechanical Engineers</publisher><subject>CIP ; Level Set ; MARS ; Propellant Management ; Sloshing ; Wave Breaking</subject><ispartof>JSME International Journal Series B Fluids and Thermal Engineering, 2004, Vol.47(4), pp.709-715</ispartof><rights>2004 by The Japan Society of Mechanical Engineers</rights><rights>Copyright Japan Science and Technology Agency 2004</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c582t-2da759dbf561efe8c69748f6179943bdc2285b4b82ffddeac40e0fe14b5500cf3</citedby><cites>FETCH-LOGICAL-c582t-2da759dbf561efe8c69748f6179943bdc2285b4b82ffddeac40e0fe14b5500cf3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,1877,4010,27900,27901,27902</link.rule.ids></links><search><creatorcontrib>HIMENO, Takehiro</creatorcontrib><creatorcontrib>WATANABE, Toshinori</creatorcontrib><creatorcontrib>NONAKA, Satoshi</creatorcontrib><creatorcontrib>NARUO, Yoshihiro</creatorcontrib><creatorcontrib>INATANI, Yoshifumi</creatorcontrib><title>Numerical Analysis of Sloshing and Wave Breaking in a Small Vessel by CIP-LSM</title><title>JSME International Journal Series B Fluids and Thermal Engineering</title><description>For the prediction of sloshing in the propellant tank of a rocket vehicle, the preliminary investigation was conducted. The flow field in the propellant tank during the ballistic flight of the vehicle was experimentally reproduced with the sub-scale model. The lateral acceleration as large as about 0.8G was provided with a mechanical exciter and the deformation of the liquid surface in the small vessel was visualized with a high-speed camera. The sloshing phenomena were also simulated with the CFD code, called CIP-LSM. The important features of surface deformation and wave breaking were successfully reproduced in the computation.</description><subject>CIP</subject><subject>Level Set</subject><subject>MARS</subject><subject>Propellant Management</subject><subject>Sloshing</subject><subject>Wave Breaking</subject><issn>1340-8054</issn><issn>1347-5371</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2004</creationdate><recordtype>article</recordtype><recordid>eNpd0FtLwzAUB_AiCs7pmx8gIPhkZ5ImTfM4h5fBvMC8PIY0Pdk603YmnbBvb7fJBF9yQvI7B84_is4JHhAq5fUiVJAPmBgILA-iHkmYiHkiyOH2juMMc3YcnYSwwDhJeCp70ePTqgJfGu3QsNZuHcqAGoumrgnzsp4hXRfoQ38DuvGgPzcvZY00mlbaOfQOIYBD-RqNxi_xZPp4Gh1Z7QKc_dZ-9HZ3-zp6iCfP9-PRcBIbntE2poUWXBa55SkBC5lJpWCZTYmQkiV5YSjNeM7yjFpbFKANw4AtEJZzjrGxST-63M1d-uZrBaFVVRkMOKdraFZBUcmwTDHt4MU_uGhWvls0KMJSwWmapBt1tVPGNyF4sGrpy0r7tSJYbZJV22QVE6pLtuPDHV-EVs9gj7VvS-PgD7Pd0fXs_8xcewV18gN5nIMZ</recordid><startdate>2004</startdate><enddate>2004</enddate><creator>HIMENO, Takehiro</creator><creator>WATANABE, Toshinori</creator><creator>NONAKA, Satoshi</creator><creator>NARUO, Yoshihiro</creator><creator>INATANI, Yoshifumi</creator><general>The Japan Society of Mechanical Engineers</general><general>Japan Science and Technology Agency</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>KR7</scope><scope>L7M</scope></search><sort><creationdate>2004</creationdate><title>Numerical Analysis of Sloshing and Wave Breaking in a Small Vessel by CIP-LSM</title><author>HIMENO, Takehiro ; WATANABE, Toshinori ; NONAKA, Satoshi ; NARUO, Yoshihiro ; INATANI, Yoshifumi</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c582t-2da759dbf561efe8c69748f6179943bdc2285b4b82ffddeac40e0fe14b5500cf3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2004</creationdate><topic>CIP</topic><topic>Level Set</topic><topic>MARS</topic><topic>Propellant Management</topic><topic>Sloshing</topic><topic>Wave Breaking</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>HIMENO, Takehiro</creatorcontrib><creatorcontrib>WATANABE, Toshinori</creatorcontrib><creatorcontrib>NONAKA, Satoshi</creatorcontrib><creatorcontrib>NARUO, Yoshihiro</creatorcontrib><creatorcontrib>INATANI, Yoshifumi</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Civil Engineering Abstracts</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>JSME International Journal Series B Fluids and Thermal Engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>HIMENO, Takehiro</au><au>WATANABE, Toshinori</au><au>NONAKA, Satoshi</au><au>NARUO, Yoshihiro</au><au>INATANI, Yoshifumi</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Numerical Analysis of Sloshing and Wave Breaking in a Small Vessel by CIP-LSM</atitle><jtitle>JSME International Journal Series B Fluids and Thermal Engineering</jtitle><date>2004</date><risdate>2004</risdate><volume>47</volume><issue>4</issue><spage>709</spage><epage>715</epage><pages>709-715</pages><issn>1340-8054</issn><eissn>1347-5371</eissn><abstract>For the prediction of sloshing in the propellant tank of a rocket vehicle, the preliminary investigation was conducted. The flow field in the propellant tank during the ballistic flight of the vehicle was experimentally reproduced with the sub-scale model. The lateral acceleration as large as about 0.8G was provided with a mechanical exciter and the deformation of the liquid surface in the small vessel was visualized with a high-speed camera. The sloshing phenomena were also simulated with the CFD code, called CIP-LSM. The important features of surface deformation and wave breaking were successfully reproduced in the computation.</abstract><cop>Tokyo</cop><pub>The Japan Society of Mechanical Engineers</pub><doi>10.1299/jsmeb.47.709</doi><tpages>7</tpages><oa>free_for_read</oa></addata></record>
fulltext	fulltext
identifier	ISSN: 1340-8054
ispartof	JSME International Journal Series B Fluids and Thermal Engineering, 2004, Vol.47(4), pp.709-715
issn	1340-8054 1347-5371
language	eng
recordid	cdi_proquest_miscellaneous_29409602
source	J-STAGE (Japan Science & Technology Information Aggregator, Electronic) Freely Available Titles - Japanese; Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals
subjects	CIP Level Set MARS Propellant Management Sloshing Wave Breaking
title	Numerical Analysis of Sloshing and Wave Breaking in a Small Vessel by CIP-LSM
url	https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-06T05%3A17%3A42IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Numerical%20Analysis%20of%20Sloshing%20and%20Wave%20Breaking%20in%20a%20Small%20Vessel%20by%20CIP-LSM&rft.jtitle=JSME%20International%20Journal%20Series%20B%20Fluids%20and%20Thermal%20Engineering&rft.au=HIMENO,%20Takehiro&rft.date=2004&rft.volume=47&rft.issue=4&rft.spage=709&rft.epage=715&rft.pages=709-715&rft.issn=1340-8054&rft.eissn=1347-5371&rft_id=info:doi/10.1299/jsmeb.47.709&rft_dat=%3Cproquest_cross%3E29409602%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=1467526362&rft_id=info:pmid/&rfr_iscdi=true