Experimental characterization and testing of adhesive bonding for space structure applications
Author:
Affiliation:
1. Arizona State University
2. Northrop Grumman Corp
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0800
Reference9 articles.
1. Computational analysis of failure mechanisms in composite sandwich space structures subject to cyclic thermal loading
2. Kim, K.S., Yoo, J.S., Yi, Y.M. and Kim, C.G., 2006. Failure mode and strength of unidirectional composite single lap bonded joints with different bonding methods. Composite structures, 72(4), pp.477-485.
3. Jensen, R., DeSchepper, D., Flanagan, D., Chaney, W.K., Robinette, J., Chaney, G. and Pergantis, C., 2014. Adhesives: test method, group assignment, and categorization guide for highloading-rate applications. Army Research Lab Aberdeen Proving Ground Md Weapons and Materials Research Dir/Materials and Manufacturing Science Div.
4. Seong, M.S., Kim, T.H., Nguyen, K.H., Kweon, J.H. and Choi, J.H., 2008. A parametric study on the failure of bonded single-lap joints of carbon composite and aluminum. Composite structures, 86(1-3), pp.135-145.
5. Experimental study on failure mechanism of hybrid composite joints with different adhesives
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