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Link-Up Strength of 2524-T3 and 2024-T3 Aluminum Panels with Multiple Site Damage
- Source :
- Journal of Aircraft. 42:535-541
- Publication Year :
- 2005
- Publisher :
- American Institute of Aeronautics and Astronautics (AIAA), 2005.
-
Abstract
- The aluminum alloy 2524-T3 is replacing 2024-T3 for many applications because 2524-T3 has a greater fracture toughness while retaining the same strength. Much attention has been given to the effect of multiple site damage on 2024-T3 aluminum; however, very little has been reported about 2524-T3. Twenty-two panels of 2524-T3, each with a different crack configuration, were tested for critical (linkup) strength, and the results were compared with an identical set of previously tested 2024-T3 panels with MSD. The panels were 24 in. wide with a midspan row of 0.25-in.-diam holes at 1-in. pitch. Each panel had a central lead crack with collinear MSD cracks emerging from both sides of the adjacent holes. A comparison of the results showed the 2524-T3 panels to average approximately 27% greater strength than the 2024-T3 panels. The linkup or plastic-zone-touch model used to predict the critical (link-up) strength of the panels was found to be highly conservative. Consequently the test data were used for a semi-empirical analysis to develop a modified link-up model for 2524-T3, similar to the one previously developed for 2024-T3. The average error between the critical strengths from testing and those predicted by the link-up model was approximately 20%, whereas that for the modified link-up model was approximately 3%.
- Subjects :
- Materials science
Fissure
business.industry
Shell (structure)
Aerospace Engineering
chemistry.chemical_element
Structural engineering
Residual strength
Fracture toughness
medicine.anatomical_structure
chemistry
Aluminium
visual_art
Aluminium alloy
visual_art.visual_art_medium
medicine
business
Stress intensity factor
Test data
Subjects
Details
- ISSN :
- 15333868 and 00218669
- Volume :
- 42
- Database :
- OpenAIRE
- Journal :
- Journal of Aircraft
- Accession number :
- edsair.doi...........7eedb4de5ec4060e824096574abccc18
- Full Text :
- https://doi.org/10.2514/1.4211