Crump, D.A., Dulieu-Barton, J.M. and Savage, J.
Full-scale performance assessment of aircraft secondary sandwich structure using thermoelastic stress analysis
At 17th International Conference on Composite Materials (ICCM 17).
27 - 31 Jul 2007.
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.
Conference or Workshop Item
|Venue - Dates:
||17th International Conference on Composite Materials (ICCM 17), 2007-07-27 - 2007-07-31
||Composite sandwich structure, RFI, TSA, full scale testing
||Fluid Structure Interactions Group
||14 Sep 2009
||18 Apr 2017 21:23
|Further Information:||Google Scholar|
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