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 At 17th International Conference on Composite Materials (ICCM 17). 27 - 31 Jul 2007. 10 pp.

Download

[img] PDF JaniceDulieu-Barton1.pdf - Other
Download (610kB)

Description/Abstract

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)
Venue - Dates: 17th International Conference on Composite Materials (ICCM 17), 2007-07-27 - 2007-07-31
Keywords: Composite sandwich structure, RFI, TSA, full scale testing
Subjects:
Organisations: Fluid Structure Interactions Group
ePrint ID: 68659
Date :
Date Event
2009Published
Date Deposited: 14 Sep 2009
Last Modified: 18 Apr 2017 21:23
Further Information:Google Scholar
URI: http://eprints.soton.ac.uk/id/eprint/68659

Actions (login required)

View Item View Item