A review on shape memory alloys with applications to morphing aircraft
By Silvestro Barbarino, E. Flores, R. Ajaj, I. Dayyani, Michael I. Friswell. 2014
380 citations recorded by the source corpus.
Subfields: Civil and Structural Engineering, Materials Chemistry, Polymers and Plastics
View Paper: https://www.semanticscholar.org/paper/dd04e268dff42d8c35b1c033313ffd8da6ec63d7
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In Civil and Structural Engineering
In Materials Chemistry
In Polymers and Plastics
Citations in the corpus
- Buckling-induced smart applications: recent advances and trends (2015, neutral): “structure [42, 100, 104] [98, 111, 119, 121] [101, 102] [106] [28] [113, 116] [26] [156] [81, 157, 158] [124, 159, 160]”
- Reconciling viability and cost-effective shape memory alloy options – A review of copper and iron based shape memory metallic systems (2016, neutral): “The phenomena has since been observed in a number of metallic systems like Ag–Cd, Au–Cd, Cu–Al–Ni, Cu–Sn, Cu–Zn, Cu–Zn–X (X = Si, Sn, Ga, Al), In–Ti, Ni–Al, Ni–Ti, Mn–Cu, Fe– Pt, Fe–Mn–Si [3].”
- Fibre Optic Sensors for Structural Health Monitoring of Aircraft Composite Structures: Recent Advances and Applications (2015, methodology): “The application of SMAs to aircraft structures [161] includes mainly the possibility of realizing the so-called “adaptive wing” in which special actuators are used to modify the shape during flight, and control its aerodynamic and flight dynamic characteristics.”
- A review of modelling and analysis of morphing wings (2018, background): “Some of these references classified morphing wings based on the geometry change [1-3, [9] or the actuator concepts [7], while other references focused at one specific element, such as special materials and relative techniques [6,8,11,12], special actuators [10] and applications [4,5].”
- Materials that couple sensing, actuation, computation, and communication (2015, background): “SMA materials exhibit two types of effects based on temperature and load, namely a super-elastic effect and a shape memory effect [12].”
- Morphing aircraft based on smart materials and structures: A state-of-the-art review (2016, background): “…strain that can be recovered when the temperature is higher than Ms. SMA has the property of super-elasticity, which means it could work even under high applied loads and large inelastic deformations, or undergo large strains without plastic deformation or failure (Barbarino et al., 2014).”