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FE-simulations of a lap joint and a stringer run-out using adhesive joint elements.: NFFP-Project 372 Adhesive Bonding in Metal Aircraft Structures (ABIMAS). Deliverable nr: D1.5 and D1.6
Linköping University, Department of Management and Engineering, Mechanics. Linköping University, The Institute of Technology. (Peter Schmidt, Ulf Edlund, Anders Klarbring)
2002 (English)Report (Other academic)
Place, publisher, year, edition, pages
Linköping, 2002.
Series
LITH-IKP-R, ISSN 0281-5001 ; 1276
Series
Swedish National Aeronautical Research Programme(NFFP) ABIMAS-Reports, D1.5, D1.6
Keyword [en]
Adhesive Joints, Finite Element Method, Damage Mechanics, Failure simulations
National Category
Mechanical Engineering
Identifiers
URN: urn:nbn:se:liu:diva-18597OAI: oai:DiVA.org:liu-18597DiVA: diva2:220573
Projects
NFFP-Project 372 Adhesive Bonding in Metal Aircraft Structures (ABIMAS).
Available from: 2009-06-01 Created: 2009-06-01 Last updated: 2013-02-18

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Schmidt, Peter

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CiteExportLink to record
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