Detection of Damage During Quasi-Static Loading of a Single Stringer Panel Using Passive Thermography and Acoustic EmissionThe purpose of this paper is to describe the methodology of measuring damage onset and growth in a composite structure during quasi-static loading using passive thermography and acoustic emission. The early detection and measurement of damage progression is important to understand failure modes. A single stringer panel was subjected to quasi-static loading to induce deformation which resulted in the formation of damage between the stiffener flange and skin. The loading was stopped when damage growth was detected. Passive thermography and acoustic emission were used to detect damage in real-time as a function of the applied load. Of particular interest are the small transient thermographic signals resulting from damage formation which can be challenging to detect, as compared to the persistent passive thermography indications of cyclic fatigue loading. We describe a custom developed thermal inspection system for detection of composite damage during quasi-static loading. The thermal results are compared to a two-dimensional multi-layered thermal simulation based on the quadrupole method. Acoustic emission is used to further characterize the damage by comparing the acoustic emission events with the thermal imagery. Results are compared to ultrasonic measurements to document the damage through-the-thickness.
Document ID
20190000884
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Zalameda, Joseph N. (NASA Langley Research Center Hampton, VA, United States)
William, Winfree P. (NASA Langley Research Center Hampton, VA, United States)
Horne, Michael R. (National Inst. of Aerospace Hampton, VA, United States)
Date Acquired
February 21, 2019
Publication Date
June 4, 2018
Subject Category
Acoustics
Report/Patent Number
NF1676L-28532Report Number: NF1676L-28532
Meeting Information
Meeting: 2018 SEM Annual Conference and Exposition on Experimental and Applied Mechanics
Location: Greenville, SC
Country: United States
Start Date: June 4, 2018
End Date: June 7, 2018
Sponsors: Society for Experimental Mechanics, Inc.