Experimental Investigation on Thermal Degradation of Multilayer Honeycomb Core Laminate Sandwich Composite in a Cone Calorimeter

Author:

Najmi Hussain,Luche Jocelyn,Rogaume Thomas

Publisher

Springer Singapore

Reference16 articles.

1. Marsh G (2011) Bombardier throws down the gauntlet with Cseries airliner. Reinf Plast 55(6):22–26

2. Shi Y, Swait T, Soutis C (2012) Modelling damage evolution in composite laminates subjected to low velocity impact. Compos Struct 94(9):2902–2913

3. FAR 25.853 a-1. Heat release test for cabin materials. Compiled by April Hornor, Aircraft Materials Fire Test Handbook, FAA report DOT/FAA/AR-00/12, April 2000

4. Mouritz A. Fire safety of advanced composites for aircraft. ATSB Research and Analysis Report Aviation Safety Research Grant—B2004/0046 2006 April

5. Kandola BK, Horrocks AR, Padmore K, Dalton J, Owen T (2006) Comparison of cone and OSU calorimetric techniques to assess the flammability behaviour of fabrics used for aircraft interiors. Fire Mater 30:241–255

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