• Dr Rashmi Dwivedi
• Imran Saundatti

Composite materials are extensively used in aerospace industries for manufacturing aerospace parts. These parts have very high strengths and low weight. Aerospace components are subjected to impact load, fatigue load and transient load. The stiffness and strength of composite ply varies with respect to ply orientation and resin percentage used. The resistance to withstand the dynamic behavior of each lamina in the presence of resin which acts as a single core material plays a very significant role in withstanding the loads under various load conditions. The use of stress contours to calculate interlaminar von Mises stress for each ply which is placed at different orientation in structure. Mode, I fracture with increasing load are analyzed for stress contours.

Interlaminar fracture, Stress Contours, Composites material, Aerospace structures

"INTERLAMINAR FRACTURE OF AEROSPACE COMPOSITES MATERIALS", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.11, Issue 2, page no.f639-f644, February-2024, Available :http://www.jetir.org/papers/JETIR2402576.pdf

"INTERLAMINAR FRACTURE OF AEROSPACE COMPOSITES MATERIALS", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.11, Issue 2, page no. ppf639-f644, February-2024, Available at : http://www.jetir.org/papers/JETIR2402576.pdf