What is it about?
This research explores a new way to make airplane wings more adaptive and efficient by using a smart metal called Nitinol, a Shape Memory Alloy (SMA). Nitinol has a unique ability: when heated, it changes shape, and when cooled, it returns to its original form—just like how birds adjust their wings mid-flight. The project replaces traditional heavy and complex hydraulic systems with Nitinol springs to move the wing flaps. These springs expand with heat and contract when cooled, enabling smooth, controlled changes in wing shape to suit different flying conditions—like takeoff, cruising, or landing. This "morphing" improves lift, reduces drag, and can increase fuel efficiency. A key part of the study was designing a system to heat and cool the springs efficiently, using battery-powered heating and a custom cooling setup to ensure fast, repeatable movement. The design was modeled using SolidWorks and tested virtually in ANSYS for both structural strength and aerodynamic performance. Overall, the study shows that heat-activated Nitinol springs could offer a lighter, more efficient alternative to conventional aircraft control systems—bringing us closer to smarter, bird-inspired flying machines.
Featured Image
Photo by Edwin Petrus on Unsplash
Why is it important?
The most important aspect of this project is the innovative use of Nitinol springs, a type of Shape Memory Alloy (SMA), to actuate aircraft wing flaps through controlled heating and cooling. This replaces traditional hydraulic systems with a lighter, more efficient, and compact mechanism that mimics bird-like wing movement. A key achievement was designing a precise thermal management system to regulate spring actuation and reset. Simulated using ANSYS and SolidWorks, the system proved structurally sound with a high factor of safety, demonstrating its potential to enhance aerodynamic performance, fuel efficiency, and adaptability in future aircraft designs.
Perspectives
This project offered a valuable opportunity to explore the potential of smart materials in advancing aerospace technology. I was particularly intrigued by the application of Nitinol Shape Memory Alloys to enable wing morphing through controlled thermal activation. The ability of these materials to respond adaptively to external conditions reflects a nature-inspired approach to engineering that I find deeply compelling. Working on this research strengthened my understanding of thermomechanical behavior and broadened my perspective on how innovative material choices can lead to more efficient, responsive, and intelligent aerospace systems.
Swetha Santhanam
Sreenidhi Institute of Science and Technology
Working on the aircraft morphing wing project was both challenging and rewarding, especially as someone from a non-aeronautical background. I explored smart materials—particularly Nitinol—and was fascinated by its ability to return to a pre-set shape at a specific temperature (Transition temperature). This sparked my interest in exploring its potential applications, and I chose the aircraft wing, a critical yet less explored component. The goal was to reduce weight, simplify the mechanism, and lower maintenance requirements, all without compromising aerodynamic efficiency. One of the biggest hurdles was fitting the actuator mechanism within the wing while maintaining structural integrity and ensuring the Nitinol could withstand the significant loads encountered during flight. Despite limited access to high-level aircraft data, I was excited to match real-time wing profiles and configurations to my design. This project not only expanded my understanding of flight dynamics and material behavior but also reinforced the immense potential of smart materials like Nitinol in shaping the future of lightweight, efficient aerospace systems.
Aakash Chellangi
Read the Original
This page is a summary of: Design of aircraft morphing wing using shape memory alloy as an actuator, January 2025, American Institute of Physics,
DOI: 10.1063/5.0263964.
You can read the full text:
Contributors
The following have contributed to this page







