Cogent Engineering
Volume 11, 2024 - Issue 1
Mechanical Engineering
An analogy of RVE-based numerical model and experimental study of Charpy impact on thin carbon/aramid hybrid composites for micro/mini-Belly landing UAV fuselage
Sojan Andrews Zachariaha Department of Aeronautical and Automobile Engineering, Manipal Institute of Technology, Manipal Academy of Higher Education, Manipal, India;b Department of Operations and Development, Worldwide Oilfield Machine Middle East, Dubai, United Arab Emirates
https://orcid.org/0000-0002-1337-3100View further author information
https://orcid.org/0000-0002-1337-3100View further author information, Pai K. Dayanandaa Department of Aeronautical and Automobile Engineering, Manipal Institute of Technology, Manipal Academy of Higher Education, Manipal, Indiahttps://orcid.org/0000-0003-0334-8718View further author information
https://orcid.org/0000-0003-0334-8718View further author information, Padmaraj N. H.a Department of Aeronautical and Automobile Engineering, Manipal Institute of Technology, Manipal Academy of Higher Education, Manipal, Indiahttps://orcid.org/0000-0001-6626-2765View further author information
https://orcid.org/0000-0001-6626-2765View further author information & Satish Shenoy B.a Department of Aeronautical and Automobile Engineering, Manipal Institute of Technology, Manipal Academy of Higher Education, Manipal, IndiaCorrespondence[email protected]
https://orcid.org/0000-0003-2374-3854View further author information
https://orcid.org/0000-0003-2374-3854View further author information