PSI - Issue 59

Ilham Bagus Wiranto et al. / Procedia Structural Integrity 59 (2024) 230–237 Wiranto et al. / Structural Integrity Procedia 00 (2019) 000 – 000

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on structures and products that rely on such materials. The findings may help inform future composite material development, aiding in the creation of more robust and resilient materials for various applications.

c. Mass = 50 kg; speed: 7.67 m/s

b. Mass = 50 kg; speed: 6.26 m/s

a. Mass = 50 kg; speed: 4.43 m/s

f. Mass = 100 kg; speed: 7.67 m/s

d. Mass = 100 kg; speed: 4.43 m/s

e. Mass = 100 kg; speed: 6.26 m/s

h. Mass = 150 kg; speed : 6.26 m/s

i. Mass = 150 kg; speed: 7.67 m/s

g. Mass = 150 kg; speed: 4.43 m/s

Fig. 5. Deformation of composite stiffened panel at maximum displacement.

Acknowledgements This work is part of the research scope of Numerical Testing and Validation of Crashworthiness Analysis in Composite Fuselage Design of Unmanned Aerial Vehicle (UAV) in collaboration with the Department of Mechanical Engineering Universitas Sebelas Maret, Surakarta, supported by The Nanotechnology and Materials Research Organization BRIN through the Fundamental Molecular Science Research Program 2023. References

ABAQUS, 2023. Analysis User’s Manual, Version 6.23. Dassault Systèmes Simulia Corp., Rhode Islan d, Unitad States. Available: https://www.3ds.com/products-services/simulia/products/abaqus/