PDF
…Inspections
• Wave Propagation Methodology Development
• Conclusions, Benefits to Aviation, and Future Work
7
Test Specimens
Use Existing Damaged Specimens
• previously-tested specimens from FAA
project “Impact Damage Formation on
Composite Aircraft Structures”
• FrameXX panel series
– C-frame crack
– shear ties crushed
• StringerXX panel series…
https://www.wichita.edu/industry_and_defense/NIAR/Documents/UCSD_JAMSPresentation-NDE_2015.pdf