Damage Assessment by Acousto-Ultrasonic Technique in Composites

2009 ◽  
pp. 380-380-18 ◽  
Author(s):  
L Lorenzo ◽  
HT Hahn
Keyword(s):  
Damage Assessment ◽  
Ultrasonic Technique

Acousto-ultrasonic technique applied to filled-polymer damage assessment

1995 ◽  
Vol 32 (5) ◽  
pp. 866-869 ◽  
Author(s):  
B. Tang ◽  
C. T. Liu ◽  
E. G. Henneke
Keyword(s):  
Damage Assessment ◽  
Ultrasonic Technique ◽  
Filled Polymer

Creep damage assessment in titanium alloy using a nonlinear ultrasonic technique

2008 ◽  
Vol 59 (8) ◽  
pp. 818-821 ◽  
Author(s):  
Sony Baby ◽  
B. Nagaraja Kowmudi ◽  
C.M. Omprakash ◽  
D.V.V. Satyanarayana ◽  
Krishnan Balasubramaniam ◽  
...  
Keyword(s):  
Titanium Alloy ◽  
Damage Assessment ◽  
Creep Damage ◽  
Ultrasonic Technique ◽  
Nonlinear Ultrasonic

A Practical Ultrasonic Inspection Method for Detecting and Characterising Defects Found Within Composite Repairs

2018 ◽  
Author(s):  
J Downing ◽  
A Hook
Keyword(s):  
Wall Thickness ◽  
Steel Substrate ◽  
Ultrasonic Method ◽  
Ultrasonic Inspection ◽  
Heat Exposure ◽  
Matrix Cracking ◽  
Ultrasonic Technique ◽  
Inspection Method ◽  
Composite Repairs ◽  
Layered Matrix

Two steel substrate test panels were developed to represent common plate thicknesses found on naval vessels and scanned using the Babcock developed ultrasonic technique. One sample comprised of a series of slotted surface breaking flaws of varying widths and through thicknesses to represent fracturing/cracking. The inspection method detected simulated cracking to a depth of 2mm and 0.5mm in width. The second sample included numerous loss of wall thickness areas of varying diameters and through thicknesses, with the smallest detectable loss of wall thickness being 0.1mm at a 15mm diameter. After proving confidence in detection, there was a need to characterise flaws to provide support and ascertain a repair action. Samples were produced that were subjected to either impact or heat exposure to induce realistic representative damage. The practical ultrasonic method was successfully used to independently characterise between the samples, with induced de-laminations caused by blisters, and multi layered matrix cracking caused by varying levels of projectile impacts, due to their unique morphology.

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