Approximate analysis of containment/deflection ring responses to engine rotor fragment impact

The transient responses of containment and/or deflection rings to impact from an engine rotor-blade fragment are analyzed. Energy and momentum considerations are employed in an approximate analysis to predict the collision-induced velocities which are imparted to the fragment and to the affected rin...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Journal of aircraft 1973-01, Vol.10 (1), p.28-37
Hauptverfasser: Wu, Richard W.-H, Witmer, Emmett A
Format: Artikel
Sprache:eng
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 37
container_issue 1
container_start_page 28
container_title Journal of aircraft
container_volume 10
creator Wu, Richard W.-H
Witmer, Emmett A
description The transient responses of containment and/or deflection rings to impact from an engine rotor-blade fragment are analyzed. Energy and momentum considerations are employed in an approximate analysis to predict the collision-induced velocities which are imparted to the fragment and to the affected ring segment. This collision analysis is combined with the spatial finite-element representation of the ring and a temporal finite-difference solution procedure to predict the resulting large transient elastic-plastic deformations of containment/deflection rings. Some comparisons with experimental data are given.
doi_str_mv 10.2514/3.44347
format Article
fullrecord <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_crossref_primary_10_2514_3_44347</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>21995058</sourcerecordid><originalsourceid>FETCH-LOGICAL-a232t-d87d6d44df01bbefe7b4f363e02f2d82a7b2f9654ebf3f4670f1c3c5ba22f38f3</originalsourceid><addsrcrecordid>eNptkEtLAzEUhYMoWKv4F7IQxcW0mSTz6LIUX1Bwo0sJmZl7S8pMMiYZaP-9U6sbcXUX9zsHzkfIdcpmPEvlXMykFLI4IZM0EyIRZV6ekgljPE3KPF-ck4sQtoyxkhXFhHws-967nel0BKqtbvfBBOqQ1s5GbWwHNs4bwBbqaJyl3tgN9RB6ZwMEGh0FuzEWqHfReYpebw4Rarpe1_GSnKFuA1z93Cl5f3x4Wz0n69enl9VynWgueEyasmjyRsoGWVpVgFBUEkUugHHkTcl1UXFc5JmECgXKvGCY1qLOKs05ihLFlNwee8ctnwOEqDoTamhbbcENQfF0schYVo7g3RGsvQvBA6rej9v9XqVMHfQpob71jeT9kdRGa7V1gx_lhN-36htUOLRthF0c2Zv_2L-VX_ThflU</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>21995058</pqid></control><display><type>article</type><title>Approximate analysis of containment/deflection ring responses to engine rotor fragment impact</title><source>Alma/SFX Local Collection</source><creator>Wu, Richard W.-H ; Witmer, Emmett A</creator><creatorcontrib>Wu, Richard W.-H ; Witmer, Emmett A</creatorcontrib><description>The transient responses of containment and/or deflection rings to impact from an engine rotor-blade fragment are analyzed. Energy and momentum considerations are employed in an approximate analysis to predict the collision-induced velocities which are imparted to the fragment and to the affected ring segment. This collision analysis is combined with the spatial finite-element representation of the ring and a temporal finite-difference solution procedure to predict the resulting large transient elastic-plastic deformations of containment/deflection rings. Some comparisons with experimental data are given.</description><identifier>ISSN: 0021-8669</identifier><identifier>EISSN: 1533-3868</identifier><identifier>DOI: 10.2514/3.44347</identifier><language>eng</language><ispartof>Journal of aircraft, 1973-01, Vol.10 (1), p.28-37</ispartof><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a232t-d87d6d44df01bbefe7b4f363e02f2d82a7b2f9654ebf3f4670f1c3c5ba22f38f3</citedby><cites>FETCH-LOGICAL-a232t-d87d6d44df01bbefe7b4f363e02f2d82a7b2f9654ebf3f4670f1c3c5ba22f38f3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27901,27902</link.rule.ids></links><search><creatorcontrib>Wu, Richard W.-H</creatorcontrib><creatorcontrib>Witmer, Emmett A</creatorcontrib><title>Approximate analysis of containment/deflection ring responses to engine rotor fragment impact</title><title>Journal of aircraft</title><description>The transient responses of containment and/or deflection rings to impact from an engine rotor-blade fragment are analyzed. Energy and momentum considerations are employed in an approximate analysis to predict the collision-induced velocities which are imparted to the fragment and to the affected ring segment. This collision analysis is combined with the spatial finite-element representation of the ring and a temporal finite-difference solution procedure to predict the resulting large transient elastic-plastic deformations of containment/deflection rings. Some comparisons with experimental data are given.</description><issn>0021-8669</issn><issn>1533-3868</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1973</creationdate><recordtype>article</recordtype><recordid>eNptkEtLAzEUhYMoWKv4F7IQxcW0mSTz6LIUX1Bwo0sJmZl7S8pMMiYZaP-9U6sbcXUX9zsHzkfIdcpmPEvlXMykFLI4IZM0EyIRZV6ekgljPE3KPF-ck4sQtoyxkhXFhHws-967nel0BKqtbvfBBOqQ1s5GbWwHNs4bwBbqaJyl3tgN9RB6ZwMEGh0FuzEWqHfReYpebw4Rarpe1_GSnKFuA1z93Cl5f3x4Wz0n69enl9VynWgueEyasmjyRsoGWVpVgFBUEkUugHHkTcl1UXFc5JmECgXKvGCY1qLOKs05ihLFlNwee8ctnwOEqDoTamhbbcENQfF0schYVo7g3RGsvQvBA6rej9v9XqVMHfQpob71jeT9kdRGa7V1gx_lhN-36htUOLRthF0c2Zv_2L-VX_ThflU</recordid><startdate>197301</startdate><enddate>197301</enddate><creator>Wu, Richard W.-H</creator><creator>Witmer, Emmett A</creator><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>197301</creationdate><title>Approximate analysis of containment/deflection ring responses to engine rotor fragment impact</title><author>Wu, Richard W.-H ; Witmer, Emmett A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a232t-d87d6d44df01bbefe7b4f363e02f2d82a7b2f9654ebf3f4670f1c3c5ba22f38f3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1973</creationdate><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Wu, Richard W.-H</creatorcontrib><creatorcontrib>Witmer, Emmett A</creatorcontrib><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Journal of aircraft</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Wu, Richard W.-H</au><au>Witmer, Emmett A</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Approximate analysis of containment/deflection ring responses to engine rotor fragment impact</atitle><jtitle>Journal of aircraft</jtitle><date>1973-01</date><risdate>1973</risdate><volume>10</volume><issue>1</issue><spage>28</spage><epage>37</epage><pages>28-37</pages><issn>0021-8669</issn><eissn>1533-3868</eissn><abstract>The transient responses of containment and/or deflection rings to impact from an engine rotor-blade fragment are analyzed. Energy and momentum considerations are employed in an approximate analysis to predict the collision-induced velocities which are imparted to the fragment and to the affected ring segment. This collision analysis is combined with the spatial finite-element representation of the ring and a temporal finite-difference solution procedure to predict the resulting large transient elastic-plastic deformations of containment/deflection rings. Some comparisons with experimental data are given.</abstract><doi>10.2514/3.44347</doi><tpages>10</tpages></addata></record>
fulltext fulltext
identifier ISSN: 0021-8669
ispartof Journal of aircraft, 1973-01, Vol.10 (1), p.28-37
issn 0021-8669
1533-3868
language eng
recordid cdi_crossref_primary_10_2514_3_44347
source Alma/SFX Local Collection
title Approximate analysis of containment/deflection ring responses to engine rotor fragment impact
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-12T03%3A16%3A10IST&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=Approximate%20analysis%20of%20containment/deflection%20ring%20responses%20to%20engine%20rotor%20fragment%20impact&rft.jtitle=Journal%20of%20aircraft&rft.au=Wu,%20Richard%20W.-H&rft.date=1973-01&rft.volume=10&rft.issue=1&rft.spage=28&rft.epage=37&rft.pages=28-37&rft.issn=0021-8669&rft.eissn=1533-3868&rft_id=info:doi/10.2514/3.44347&rft_dat=%3Cproquest_cross%3E21995058%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=21995058&rft_id=info:pmid/&rfr_iscdi=true