Abstract

Ultrasonic testing using arrays is becoming widely used to test composite structures in the Aerospace industry. In recent years, the Full Matrix Capture (FMC) technique has been implemented to extract the signals for post-processing to form an image. The inherent anisotropy and the layering of the structure pose challenges for the interpretation of this FMC data. To overcome this challenge, modeling techniques are required that take into account the diffraction caused by finite-size transducers and the response of the structure to these bounded beams. Existing models either homogenize the entire structure, use computationally expensive finite difference time domain (FDTD) methods, or do not consider the shape of the bounded beam, which is used to test such structures. This paper proposes a modeling technique based on combining the Multi-Gaussian beam model with the recursive stiffness matrix method to simulate the FMC signals for layered anisotropic media. The paper provides the steps required for the modeling technique, the extraction of the system efficiency factor, and validation of the model with experimentally determined signals for aluminum as an isotropic material such as aluminum and Carbon Fiber Reinforced Plastic (CFRP) laminate as a layered material. The proposed method is computationally inexpensive, shows good agreement with the experimentally determined FMC data, and enables us to understand the effects of various transducer and material parameters on the extracted FMC signals.

Highlights

  • In recent years, the use of composite materials in aerospace structures has risen significantly [1,2].These structures mainly consist of multi-layered composite laminates

  • There is a need for computational models to simulate, analyze, and study the interaction of finite beam transducers with such multi-layered composite materials, taking into account the effects of multiple reflections and direction-dependent velocity

  • The novelty of the paper lies in the development of an analytical model based on the angular decomposition of multi-Gaussian beams combined with the response of the laminate to simulate the full matrix capture (FMC) signals

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Summary

Introduction

The use of composite materials in aerospace structures has risen significantly [1,2]. To simulate the signals obtained while testing a structure, it is necessary to develop a model that is computationally inexpensive and couples the diffraction effect of the beam from the rectangular transducer element with the response of the structure under consideration. The novelty of the paper lies in the development of an analytical model based on the angular decomposition of multi-Gaussian beams combined with the response of the laminate to simulate the full matrix capture (FMC) signals. This model uses multi-Gaussian beams to represent the source beam combined with an experimentally determined system function and the total reflection coefficient of the material under inspection calculated using the recursive stiffness matrix method.

Carbon
Modeling of the Transducer Gaussian Beams
Angular Spectrum of Plane Waves
Modeling of Array Signals to Simulate FMC
Simulation and Experimental Results
Elements
Total Reflection Coefficient of the Materials under Inspection
System Functions of the Transducer Arrays
MHz for testing
Comparison of Experimental and Simulated FMC Signals
Experimental and Simulated FMC Signals in Aluminum
MHz element array
Experimental and Simulated Signals in CFRP
Findings
Conclusions
Full Text
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