Prediction of Thermal Expansion Properties of Carbon/Epoxy Laminates for Temperature Variation
This paper is concerned with the prediction of coefficients of thermal expansion (CTE) of Carbon/Epoxy laminates for temperature variation. Elastic properties and coefficients of thermal expansion in the material principal directions were measured in the range of room temperature to cure temperature...
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Veröffentlicht in: | Journal of composite materials 2000-01, Vol.34 (2), p.90-100 |
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description | This paper is concerned with the prediction of coefficients of thermal expansion (CTE) of Carbon/Epoxy laminates for temperature variation. Elastic properties and coefficients of thermal expansion in the material principal directions were measured in the range of room temperature to cure temperature and characterized as functions of temperature. By applying the characterized properties to the classical lamination theory, a computational method to predict the change of CTEs of a general laminate for temperature variation was proposed. The coefficients of thermal expansion of various angle-ply laminates were measured and compared with those predicted. Experimental results show that the changes of CTEs of a general laminate for temperature variation can be predicted well by using the proposed method. |
doi_str_mv | 10.1177/002199830003400201 |
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Joon ; Kim, Ju-Sik</creator><creatorcontrib>Yoon, K. Joon ; Kim, Ju-Sik</creatorcontrib><description>This paper is concerned with the prediction of coefficients of thermal expansion (CTE) of Carbon/Epoxy laminates for temperature variation. Elastic properties and coefficients of thermal expansion in the material principal directions were measured in the range of room temperature to cure temperature and characterized as functions of temperature. By applying the characterized properties to the classical lamination theory, a computational method to predict the change of CTEs of a general laminate for temperature variation was proposed. The coefficients of thermal expansion of various angle-ply laminates were measured and compared with those predicted. Experimental results show that the changes of CTEs of a general laminate for temperature variation can be predicted well by using the proposed method.</description><identifier>ISSN: 0021-9983</identifier><identifier>EISSN: 1530-793X</identifier><identifier>DOI: 10.1177/002199830003400201</identifier><identifier>CODEN: JCOMBI</identifier><language>eng</language><publisher>Thousand Oaks, CA: SAGE Publications</publisher><subject>Aircraft industry. Spacecraft ; Applications ; Applied sciences ; Engineering techniques in metallurgy. Applications. Other aspects ; Exact sciences and technology ; Metals. 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Joon</creatorcontrib><creatorcontrib>Kim, Ju-Sik</creatorcontrib><title>Prediction of Thermal Expansion Properties of Carbon/Epoxy Laminates for Temperature Variation</title><title>Journal of composite materials</title><description>This paper is concerned with the prediction of coefficients of thermal expansion (CTE) of Carbon/Epoxy laminates for temperature variation. Elastic properties and coefficients of thermal expansion in the material principal directions were measured in the range of room temperature to cure temperature and characterized as functions of temperature. By applying the characterized properties to the classical lamination theory, a computational method to predict the change of CTEs of a general laminate for temperature variation was proposed. The coefficients of thermal expansion of various angle-ply laminates were measured and compared with those predicted. Experimental results show that the changes of CTEs of a general laminate for temperature variation can be predicted well by using the proposed method.</description><subject>Aircraft industry. Spacecraft</subject><subject>Applications</subject><subject>Applied sciences</subject><subject>Engineering techniques in metallurgy. Applications. Other aspects</subject><subject>Exact sciences and technology</subject><subject>Metals. 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Metallurgy</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Yoon, K. Joon</creatorcontrib><creatorcontrib>Kim, Ju-Sik</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Materials Research Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Journal of composite materials</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Yoon, K. Joon</au><au>Kim, Ju-Sik</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Prediction of Thermal Expansion Properties of Carbon/Epoxy Laminates for Temperature Variation</atitle><jtitle>Journal of composite materials</jtitle><date>2000-01</date><risdate>2000</risdate><volume>34</volume><issue>2</issue><spage>90</spage><epage>100</epage><pages>90-100</pages><issn>0021-9983</issn><eissn>1530-793X</eissn><coden>JCOMBI</coden><abstract>This paper is concerned with the prediction of coefficients of thermal expansion (CTE) of Carbon/Epoxy laminates for temperature variation. Elastic properties and coefficients of thermal expansion in the material principal directions were measured in the range of room temperature to cure temperature and characterized as functions of temperature. By applying the characterized properties to the classical lamination theory, a computational method to predict the change of CTEs of a general laminate for temperature variation was proposed. The coefficients of thermal expansion of various angle-ply laminates were measured and compared with those predicted. Experimental results show that the changes of CTEs of a general laminate for temperature variation can be predicted well by using the proposed method.</abstract><cop>Thousand Oaks, CA</cop><pub>SAGE Publications</pub><doi>10.1177/002199830003400201</doi><tpages>11</tpages></addata></record> |
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subjects | Aircraft industry. Spacecraft Applications Applied sciences Engineering techniques in metallurgy. Applications. Other aspects Exact sciences and technology Metals. Metallurgy |
title | Prediction of Thermal Expansion Properties of Carbon/Epoxy Laminates for Temperature Variation |
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