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Computational Non-Destructive Evaluation Improving Ultrasonic Interrogation of Complex Geometry Composite PartsFinite element simulation was employed in modeling the ultrasound (UT) pressure pulse propagation through a coupled liquid-composite medium to reproduce experimental data. From the simulation point of view, the proposed approach is challenging when there is a large simulation domain. For example, it is shown that a sub-micron wavelength of an ultrasonic wave requires a mesh size of several microns and this in turn requires significant computational resources, as well as special care in modeling. Some of the simulation results are presented considering that such modeling should reproduce experimental data for a healthy and faulty composite structure with complex geometry. Many possible experimental setups are simulated to demonstrate the non-destructive testing technique. This setup includes the generation of pressure pulse propagating through the tested composite plate and possible scattering by discontinuities (area of different impedance) that may be present in the panel. This scattered pulse together with the baseline pressure pulse generates a signature on the probe element which can be used to locate the position of defects in the structures.
Document ID
20190026438
Acquisition Source
Ames Research Center
Document Type
Technical Memorandum (TM)
Authors
Hafiychuk, V.
(Stinger Ghaffarian Technologies Inc. (SGT Inc.) Moffett Field, CA, United States)
Wheeler, K. R.
(NASA Ames Research Center Moffett Field, CA, United States)
Gee, K.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
June 18, 2019
Publication Date
March 1, 2019
Subject Category
Mechanical Engineering
Report/Patent Number
ARC-E-DAA-TN67907
NASA/TM-2019-220197
Report Number: ARC-E-DAA-TN67907
Report Number: NASA/TM-2019-220197
Funding Number(s)
CONTRACT_GRANT: NNA14AA60C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
modeling
waves
ultrasound
NDE
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