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Sensor-Based Structural Health Monitoring of Composite Laminates Under Low-Velocity Impact

Sensor-Based Structural Health Monitoring Composite is a M.Tech project topic for Aerospace Engineering. Explore the IEEE-style abstract, reference…

Sensor-Based Structural Health Monitoring Composite is a M.Tech project topic for Aerospace Engineering. It gives students a clear starting point for research, implementation planning, and documentation.

Sensor-Based Structural Health Monitoring Composite Project Details

Abstract

This research investigates a sensor-based structural health monitoring (SHM) framework for carbon-fiber-reinforced polymer (CFRP) panels subjected to low-velocity impacts. Such impacts, common during manufacturing and maintenance, can induce barely visible impact damage (BVID) in composite aircraft structures, necessitating advanced assessment techniques. The proposed methodology integrates surface-mounted strain gauges with explicit finite element analysis (FEA) to enable rapid post-event evaluation. Experimental validation involved drop-weight tests on CFRP laminates, adhering to ASTM D7136 standards, utilizing a 1.0 kg hemispherical impactor across varying drop heights. Strain gauges strategically positioned relative to the impact point quantified the spatial attenuation of peak surface strain. Results indicated a clear impact energy-dependent decay in peak strains, with

a notable deviation from elastic energy scaling at higher impact energies, signifying a transition to damage-dominated energy dissipation. Dedicated numerical simulations, employing MSC Apex/Nastran Implicit, successfully replicated experimental trends, establishing a physics-based digital twin for interpreting elastic strain signatures and correlating them with probable damage states.

Reference Paper Sensor-Based Structural Health Monitoring of Composite Laminates Under Low-Velocity Impact
Domain Aerospace Engineering
Sub-Domain Structures & Systems / Aerospace Structures / Composite Airframes
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