Investigating the Ability of Process Parameters to Reduce Defects during the Drilling of Carbon-Fiber-Reinforced Plastic (CFRP) and Aluminum Stack
Author:
Affiliation:
1. Department of Industrial Engineering, University of Engineering and Technology Taxila, Punjab 47050, Pakistan
Publisher
MDPI
Link
https://www.mdpi.com/2673-4591/45/1/53/pdf
Reference7 articles.
1. Gonczy, S.T. (2014, January 4–6). Federal Aviation Administration (FAA) airworthiness certification for ceramic matrix composite components in civil aircraft systems. Proceedings of the Testing and Modeling Ceramic & Carbon Matrix Composites, Paris, France.
2. Tool wear and hole quality in drilling of CFRP/AA7075 stacks with DLC and nanocomposite TiAlN coated tools;Forcellese;J. Manuf. Process.,2017
3. Study of drilling of composite material and aluminium stack;Zitoune;Compos. Struct.,2010
4. D’Orazio, A., Mehtedi, M.E., Forcellese, A., Nardinocchi, A., and Simoncini, M. (2018, January 23–25). Study of tapping process of carbon fiber reinforced plastic composites/AA7075 stacks. Proceedings of the 21st International ESAFORM Conference on Material Forming (ESAFORM 2018), Palermo, Italy.
5. Evaluation of microstructure and mechanical properties of squeeze overcast Al7075− Cu composite joints;Hanif;China Foundry,2023
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