Comparative study of composite scarf and strap joints for equivalent repair signature under uniaxial tension
Scarf joints are preferred in aerospace composite repairs that offer better strength, flushed surface and nearly uniform shear and peel stress distribution along the bond length. However, a shallow scarf angle repair of 2° to 3° as practiced requires significant parent material removal thus increasi...
Saved in:
Main Authors: | Srinivasan, Dharun Vadugappatty, Padma, S. Ravisankar, Idapalapati, Sridhar |
---|---|
Other Authors: | School of Mechanical and Aerospace Engineering |
Format: | Article |
Language: | English |
Published: |
2022
|
Subjects: | |
Online Access: | https://hdl.handle.net/10356/162455 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Nanyang Technological University |
Language: | English |
Similar Items
-
Thermo-mechanical debonding map for repairing composite–metal adhesive joints
by: Srinivasan, Dharun Vadugappatty, et al.
Published: (2021) -
Effect of scarf repair geometry on the impact performance of aerospace composites
by: Shankar, Sridharan Vijay, et al.
Published: (2023) -
Failure analysis of GFRP single lap joints tailored with a combination of tough epoxy and hyperelastic adhesives
by: Srinivasan, Dharun Vadugappatty, et al.
Published: (2020) -
Effect of residual epoxy on single lap joints performance
by: Srinivasan, Dharun Vadugappatty, et al.
Published: (2020) -
Temperature-dependent peel performance of adhesively rebonded hybrid joints
by: Srinivasan, Dharun Vadugappatty, et al.
Published: (2020)