• Akshay
• Rajesh Kumar
• Ravinder Kundu

This study presents the Experimental characterizations of composite sandwich structures needed to optimize structure design. We fabricated composite sandwich structures; one is having a Nomex Honeycomb Core of 5mm thickness and another having a Nomex Honeycomb Core of 8 mm thickness. Honeycomb sandwich panels had Carbon and fiber face sheets (3 layers of Carbon of .2 mm each). The mechanical properties of the constituent materials were discovered experimentally using ASTM/ISO standards. After testing a comparison is made of the different properties achieved from the two different specimen having core thickness of 5 mm and 8 mm. By analysis it was observed with the core height (5 mm) when span length is increased the flexural strength increases and with the core height (8 mm) when span length is increased the flexural strength decreases.

Composites, Nomex Honeycomb, Mechanical properties, Flexural Test

"Fabrication and 3 Point Bending Analysis of Nomex Composite Sandwich Panel", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.6, Issue 6, page no.116-121, June-2019, Available :http://www.jetir.org/papers/JETIR1907S86.pdf

"Fabrication and 3 Point Bending Analysis of Nomex Composite Sandwich Panel", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.6, Issue 6, page no. pp116-121, June-2019, Available at : http://www.jetir.org/papers/JETIR1907S86.pdf