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Meta-Isolators: Advanced Metamaterial Solutions for Low-Frequency Vibration Control in Aerospace Structures

Implementing Organization

Indian Institute of Science
Principal Investigator
Dr. Abhigna Sandipkumar Bhatt
Indian Institute Of Science
abhigna.bhatt@gmail.com

Project Overview

This research project aims to develop novel metamaterial-based vibration isolators specifically designed for aerospace applications. The project focuses on creating advanced low-frequency vibration control solutions for critical aerospace structural components including sandwich beams, plates, and shells. Metamaterials, with their engineered periodic structures, enable extraordinary functionalities such as vibration isolation and wave manipulation through their structural architecture rather than intrinsic material properties. The project introduces innovative "meta-isolators" that integrate three metamaterial mechanisms: negative effective mass, negative effective stiffness, and inertial amplification. This combination enables unprecedented low-frequency bandgap performance while maintaining the lightweight characteristics essential for aerospace applications. Unlike conventional vibration control methods that often require heavy masses and low stiffness, this approach addresses the critical challenge of achieving wide and low-frequency bandgaps without significant weight penalties. The research methodology encompasses four interconnected work packages that systematically progress from theoretical foundations to practical implementation. Mathematical modeling forms the cornerstone, utilizing spectral element methods and rigid body dynamics to develop advanced analytical models for accurate wave dispersion analysis. The approach integrates metamaterial mechanisms into aerospace structural components to achieve tunable low-frequency bandgaps, with closed-form expressions derived for vibration transmittance characteristics including band edges and attenuation peaks. Design optimization employs multi-objective techniques including topology optimization and genetic algorithms to achieve minimal weight, compactness, and maximum broadband vibration isolation performance. Numerical validation using Wave Finite Element Methods and reduced-order modeling ensures the reliability of analytical predictions under realistic boundary conditions. The experimental phase involves prototype fabrication through additive manufacturing and comprehensive testing using advanced measurement techniques such as Laser Doppler Vibrometry. The project addresses critical vibration control needs in aerospace systems including satellite communication platforms, precision navigation instruments, and aircraft structures. The developed meta-isolators will protect sensitive components, maintain structural integrity, and prevent mechanical fatigue while offering significant advantages over conventional solutions. This research bridges the gap between theoretical metamaterial concepts and practical aerospace applications, potentially revolutionizing vibration control in next-generation aerospace systems.
Funding Organization
Funding Organization
Anusandhan National Research Foundation (ANRF)
Quick Information
Area of Research
Engineering Sciences
Focus Area
Mechanical Engineering
Start Date
11 Nov 2025
End Date
10 Nov 2027
Status
ongoing
Output
No. of Research Paper
00
Technologies (If Any)
00
No. of PhD Produced
00
Publications
00
No. of Patents
Filed : 00
Grant : 00
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