Full-scale performance assessment of aircraft secondary sandwich structure using thermoelastic stress analysis
Crump, D.A., Dulieu-Barton, J.M. and Savage, J. (2009) Full-scale performance assessment of aircraft secondary sandwich structure using thermoelastic stress analysis. In, 17th International Conference on Composite Materials (ICCM 17), Edinburgh, UK, 27 - 31 Jul 2007. London, UK, IOM Communications10pp.
The use of resin film infusion (RFI) has been proven to reduce the cost of production of aircraft secondary sandwich structure. In this paper thermoelastic stress analysis (TSA) is used to assess the performance of full scale aircraft sandwich structure panels produced using both the conventional autoclave process and RFI. Finite element (FE) models of both panel types are developed and TSA is used to validate the models.
|Item Type:||Conference or Workshop Item (Paper)|
|Keywords:||Composite sandwich structure, RFI, TSA, full scale testing|
|Subjects:||T Technology > TJ Mechanical engineering and machinery
Q Science > QC Physics
|Divisions:||University Structure - Pre August 2011 > School of Engineering Sciences
University Structure - Pre August 2011 > School of Engineering Sciences > Fluid-Structure Interactions
|Date Deposited:||14 Sep 2009|
|Last Modified:||08 Jun 2012 12:30|
|Contributors:||Crump, D.A. (Author)
Dulieu-Barton, J.M. (Author)
Savage, J. (Author)
|RDF:||RDF+N-Triples, RDF+N3, RDF+XML, Browse.|
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