Specimen TC-24-31-2
Readme
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| Description | Summary of information about specimen and dataset organization and datatypes. |
Experimental Photos
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| Description | Photos taken during impact and residual strength testing. |
Impact Summary
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| Description | Force-history loading curve data from impact testing. |
| Technical Details | Pendulum impactor with a 25.4 mm radius metal tip. Specimen TC-24-31-2 impacted at 24.1 J. |
Ultrasonic pulse-echo testing
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| Description | Ultrasonic pulse-echo scan data presented as A-scan wave forms (.mat format) and as processed Time-of-Flight and Amplitude C-scan images. |
| Technical Details | NASA Langley floating UT system, 5 MHz transducer water column scan. |
X-ray CT scan image stack
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| Description | X-ray computed tomography scan data as a collection of TIF images of orthogonal slices. |
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| Technical Details | CT system with a Varian PaxScan 4030E detector array with an excitation voltage of 70 kV and current of 85 µA |
X-ray CT scan radiographs and VGStudio Project File
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| Description | X-ray computed tomography scan data including collected X-ray images (.att) and VGStudio formatted project files (.raw). |
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Residual strength load data
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| Description | Compression loading curves from CAI testing. |
Residual strength digital image correlation images
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| Description | DIC images collected for the front, back, and global camera pairs. |
Residual strength digital image correlation processed output
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| Description | Processed displacement and strain fields from DIC images. Provided as a Vic3D project file and as a Matlab dataset (.mat). |
- Collection
- Cite This Work
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Ellison, Andrew C.; Kim, Hyonny (2020). Specimen TC-24-31-2. In Flat Panel Impact and Residual Strength Testing and Characterization by Ultrasonic and X-Ray Computed Tomography Non-Destructive Evaluation. UC San Diego Library Digital Collections. https://doi.org/10.6075/J0HQ3XB4
- Description
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This specimen dataset includes impact, CT and UT NDE, and residual strength testing results.
- Creation Date
- 2017-07 to 2017-09
- Date Issued
- 2020
- Principal Investigator
- Researcher
- Technical Details
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24.1 J impact with a 25.4 mm radius impactor. 101.6 x 152.4 mm specimen dimensions. T800S/3900-2B unidirectional prepreg with a 24 ply [0/45/90/-45]3s layup. Additional fiberglass woven ply and aircraft grade paint on impact side. 76.2 x 101.6 mm picture frame impact window.
- Topics
Formats
View formats within this collection
- Language
- English
- Identifier
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Identifier: Andrew Ellison: https://orcid.org/0000-0002-1538-4380
- Related Resource
- Ellison, A., & Kim, H. (2018). Computed tomography informed composite damage state model generation. Journal of Composite Materials, 52(25), 3523-3538. https://doi.org/10.1177/0021998318773464
Primary associated publication
- License
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Creative Commons Attribution 4.0 International Public License
- Rights Holder
- UC Regents
- Copyright
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Under copyright (US)
Use: This work is available from the UC San Diego Library. This digital copy of the work is intended to support research, teaching, and private study.
Constraint(s) on Use: This work is protected by the U.S. Copyright Law (Title 17, U.S.C.). Use of this work beyond that allowed by "fair use" or any license applied to this work requires written permission of the copyright holder(s). Responsibility for obtaining permissions and any use and distribution of this work rests exclusively with the user and not the UC San Diego Library. Inquiries can be made to the UC San Diego Library program having custody of the work.
- Digital Object Made Available By
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Research Data Curation Program, UC San Diego, La Jolla, 92093-0175 (https://lib.ucsd.edu/rdcp)
- Last Modified
2023-06-06