Affiliation:
1. Department of Aerospace Engineering, Khalifa University of Science and Technology, Abu Dhabi 127788, United Arab Emirates
2. Advanced Research and Innovation Center (ARIC), Department of Aerospace Engineering, Khalifa University of Science and Technology, Abu Dhabi 127788, United Arab Emirates
Abstract
The use of elastomer-based skins in morphing wings has become increasingly popular due to their remarkable stretchability and mechanical properties. However, the possibility of the skin fracturing during multiaxial stretching remains a significant design challenge. The propagation of cracks originating from flaws or notches in the skin can lead to the specimen breaking into two parts. This paper presents an experimental study aimed at comprehensively evaluating crack propagation direction, stretchability, and fracture toughness of silicone-based elastomeric skin (Ecoflex) for morphing wing applications, using varying Shore hardness values (10, 30, and 50). The findings show that the lower Shore hardness value of 10 exhibits a unique Sideways crack propagation characteristic, which is ideal for morphing skins due to its high stretchability, low actuation load, and high fracture toughness. The study also reveals that the Ecoflex 10 is suitable for use in span morphing, with a fracture toughness of approximately 1.1 kJ/m2 for all thicknesses at a slower strain rate of 0.4 mm/min. Overall, this work highlights the superior properties of Ecoflex 10 and its potential use as a morphing skin material, offering a groundbreaking solution to the challenges faced in this field.
Funder
Abu Dhabi Education Council
Subject
Polymers and Plastics,General Chemistry
Reference37 articles.
1. Rivero, A.E., Fournier, S., Heeb, R.M., and Woods, B.K. (2022). Design, Manufacture and Wind Tunnel Test of a Modular FishBAC Wing with Novel 3D Printed Skins. Appl. Sci., 12.
2. Aeroelasticity of compliant span morphing wings;Ajaj;Smart Mater. Struct.,2018
3. Bishay, P.L., Burg, E., Akinwunmi, A., Phan, R., and Sepulveda, K. (2019). Development of a new span-morphing wing core design. Designs, 3.
4. The Adaptive Aspect Ratio morphing wing: Design concept and low fidelity skin optimization;Woods;Aerosp. Sci. Technol.,2015
5. A morphing wing with cellular structure of non-uniform density;Zhang;Smart Mater. Struct.,2021
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