• Akshay kumar T S
• Dr. B. M. Rajaprakash

The structural materials to be used for aerospace applications should have good strength and modulus to withstand heavy loads and also should be light enough to fly/take-off. The material that best fits to these specifications is composite materials; Carbon Fiber Reinforced Polymers (CFRP) have been used in the aerospace application as carbon fibers have very high modulus and also withstand high loads. M50J is a type of carbon fiber that is reinforced with a resin which can be cured and used as CFRP structures. A representative volume element is designed and is analysed to evaluate the performances of this material in tension, compression and shear.

Carbon fibers, Aerospace Materials, High Modulus Carbon Fiber, Analysis

"Design and Analysis of Representative Volume Element in respect of M50J Carbon Fiber Reinforce Polymer for Aerospace Application", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.6, Issue 6, page no.450-464, June 2019, Available :http://www.jetir.org/papers/JETIR1908678.pdf

"Design and Analysis of Representative Volume Element in respect of M50J Carbon Fiber Reinforce Polymer for Aerospace Application", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.6, Issue 6, page no. pp450-464, June 2019, Available at : http://www.jetir.org/papers/JETIR1908678.pdf