• Shashikumar. S
• Indu Venkat
• Manisha A Hammagi
• Poojitha D A
• Sharan Prakash

This thesis focuses on experience with adhesively bonded joints in aircraft structures. Adhesively bonded joints are used in the assembling of structural parts, especially of those which are made from dissimilar materials. These joints consists of adhesive layer and adherends with different mechanical and thermal properties. Some imperfections like holes, thermal residue stresses occurring in the bolted, welded, riveted and soldering joints don’t take place in these joints. So the main advantages of bonded joints are lightness, sealing, corrosion resistance, heat and sound isolation, damping and quickly mounting facility which is proved. This thesis introduces an attempt to study the debond analysis of adhesively bonded joints. Single lap joints having failure at the interface of adherent and adhesive are modeled in MSc Nastran software. The coordination of the experimental and numerical techniques makes it possible to find an efficient tool for studying the debond performance of adhesively bonded joints.

"ANALYSIS OF ADHESIVELY BONDED JOINTS IN AIRCRAFT STRUCTURE", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.6, Issue 5, page no.166-170, May-2019, Available :http://www.jetir.org/papers/JETIR1905E25.pdf

"ANALYSIS OF ADHESIVELY BONDED JOINTS IN AIRCRAFT STRUCTURE", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.6, Issue 5, page no. pp166-170, May-2019, Available at : http://www.jetir.org/papers/JETIR1905E25.pdf