• Trideep Kalwar
• Suresh Devkate
• Vaibhav Karpe
• Tushar Ghule
• C.S. Khemkar

In aircraft design, safety is paramount. As a result, the designer must consider the aircraft structure's safety, and in order to demonstrate that safety, the designer must first comprehend the structure's behaviour and load. Aircraft design is distinct from analytical disciplines like aerodynamics, structures, controls, and propulsion in the field of aeronautical engineering. Front fuselage, centre fuselage, and rare fuselage are the three types of fuselage in an aeroplane frame. A centre The fuselage of a conventional transport air ship is the section that houses the passengers and cargo. The ANSYS 19 workbench and CATIA R5 V20 will be used in this project to do vibration analysis of 3D modelling of fuselage panels.

Fibre glass, FEA, Catia R5 V20, ANSYS.

"DESIGN AND WEIGHT OPTIMIZATION OF AIRCRAFT FUSELAGE PANEL USING FEA AND UTM", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.9, Issue 5, page no.l45-l50, May-2022, Available :http://www.jetir.org/papers/JETIR2205C07.pdf

"DESIGN AND WEIGHT OPTIMIZATION OF AIRCRAFT FUSELAGE PANEL USING FEA AND UTM", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.9, Issue 5, page no. ppl45-l50, May-2022, Available at : http://www.jetir.org/papers/JETIR2205C07.pdf