Experiments on Pulse Propagation in an Obliquely Laminated Composite
Experimental results are presented for the linear elastic dynamic response of periodically laminated composites. A shock tube-capacitive transducer technique is used to determine the rear surface velocity history of three laminated samples that have different lamination angles and are subjected to a...
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Report |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | |
|---|---|
| container_issue | |
| container_start_page | |
| container_title | |
| container_volume | |
| creator | Sve,Charles Okubo,Seichi |
| description | Experimental results are presented for the linear elastic dynamic response of periodically laminated composites. A shock tube-capacitive transducer technique is used to determine the rear surface velocity history of three laminated samples that have different lamination angles and are subjected to a step pressure loading. Viscosity effects are discussed, and comparisons are made with predictions based on previous theoretical work. (Author-PL) |
| format | Report |
| fullrecord | <record><control><sourceid>dtic_1RU</sourceid><recordid>TN_cdi_dtic_stinet_AD0777577</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>AD0777577</sourcerecordid><originalsourceid>FETCH-dtic_stinet_AD07775773</originalsourceid><addsrcrecordid>eNrjZHBxrShILcrMTc0rKVbIz1MIKM0pTlUIKMovSExPLMkEimTmKSTmKfgn5WQWlqbmVCr4JOZm5iWWpKYoOOfnFuQXZ5ak8jCwpiUC9fFCaW4GGTfXEGcP3ZSSzOT44pLMvNSSeEcXA3Nzc1Nzc2MC0gC8IC_x</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>report</recordtype></control><display><type>report</type><title>Experiments on Pulse Propagation in an Obliquely Laminated Composite</title><source>DTIC Technical Reports</source><creator>Sve,Charles ; Okubo,Seichi</creator><creatorcontrib>Sve,Charles ; Okubo,Seichi ; AEROSPACE CORP EL SEGUNDO CALIF LAB OPERATIONS</creatorcontrib><description>Experimental results are presented for the linear elastic dynamic response of periodically laminated composites. A shock tube-capacitive transducer technique is used to determine the rear surface velocity history of three laminated samples that have different lamination angles and are subjected to a step pressure loading. Viscosity effects are discussed, and comparisons are made with predictions based on previous theoretical work. (Author-PL)</description><language>eng</language><subject>Aluminum alloys ; Composite materials ; Laminates ; Laminates and Composite Materials ; Loads(Forces) ; Plastics ; Sandwich construction ; Shock tubes ; Steel ; Stresses</subject><creationdate>1974</creationdate><rights>APPROVED FOR PUBLIC RELEASE</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,780,885,27566,27567</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/AD0777577$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Sve,Charles</creatorcontrib><creatorcontrib>Okubo,Seichi</creatorcontrib><creatorcontrib>AEROSPACE CORP EL SEGUNDO CALIF LAB OPERATIONS</creatorcontrib><title>Experiments on Pulse Propagation in an Obliquely Laminated Composite</title><description>Experimental results are presented for the linear elastic dynamic response of periodically laminated composites. A shock tube-capacitive transducer technique is used to determine the rear surface velocity history of three laminated samples that have different lamination angles and are subjected to a step pressure loading. Viscosity effects are discussed, and comparisons are made with predictions based on previous theoretical work. (Author-PL)</description><subject>Aluminum alloys</subject><subject>Composite materials</subject><subject>Laminates</subject><subject>Laminates and Composite Materials</subject><subject>Loads(Forces)</subject><subject>Plastics</subject><subject>Sandwich construction</subject><subject>Shock tubes</subject><subject>Steel</subject><subject>Stresses</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1974</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZHBxrShILcrMTc0rKVbIz1MIKM0pTlUIKMovSExPLMkEimTmKSTmKfgn5WQWlqbmVCr4JOZm5iWWpKYoOOfnFuQXZ5ak8jCwpiUC9fFCaW4GGTfXEGcP3ZSSzOT44pLMvNSSeEcXA3Nzc1Nzc2MC0gC8IC_x</recordid><startdate>19740131</startdate><enddate>19740131</enddate><creator>Sve,Charles</creator><creator>Okubo,Seichi</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>19740131</creationdate><title>Experiments on Pulse Propagation in an Obliquely Laminated Composite</title><author>Sve,Charles ; Okubo,Seichi</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_AD07775773</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1974</creationdate><topic>Aluminum alloys</topic><topic>Composite materials</topic><topic>Laminates</topic><topic>Laminates and Composite Materials</topic><topic>Loads(Forces)</topic><topic>Plastics</topic><topic>Sandwich construction</topic><topic>Shock tubes</topic><topic>Steel</topic><topic>Stresses</topic><toplevel>online_resources</toplevel><creatorcontrib>Sve,Charles</creatorcontrib><creatorcontrib>Okubo,Seichi</creatorcontrib><creatorcontrib>AEROSPACE CORP EL SEGUNDO CALIF LAB OPERATIONS</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Sve,Charles</au><au>Okubo,Seichi</au><aucorp>AEROSPACE CORP EL SEGUNDO CALIF LAB OPERATIONS</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Experiments on Pulse Propagation in an Obliquely Laminated Composite</btitle><date>1974-01-31</date><risdate>1974</risdate><abstract>Experimental results are presented for the linear elastic dynamic response of periodically laminated composites. A shock tube-capacitive transducer technique is used to determine the rear surface velocity history of three laminated samples that have different lamination angles and are subjected to a step pressure loading. Viscosity effects are discussed, and comparisons are made with predictions based on previous theoretical work. (Author-PL)</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng |
| recordid | cdi_dtic_stinet_AD0777577 |
| source | DTIC Technical Reports |
| subjects | Aluminum alloys Composite materials Laminates Laminates and Composite Materials Loads(Forces) Plastics Sandwich construction Shock tubes Steel Stresses |
| title | Experiments on Pulse Propagation in an Obliquely Laminated Composite |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-12T20%3A07%3A44IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-dtic_1RU&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=unknown&rft.btitle=Experiments%20on%20Pulse%20Propagation%20in%20an%20Obliquely%20Laminated%20Composite&rft.au=Sve,Charles&rft.aucorp=AEROSPACE%20CORP%20EL%20SEGUNDO%20CALIF%20LAB%20OPERATIONS&rft.date=1974-01-31&rft_id=info:doi/&rft_dat=%3Cdtic_1RU%3EAD0777577%3C/dtic_1RU%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |