Finite Element Analysis of a Flapping Dragonfly Wing
Faculty Mentor
Dr. Mosfequr Rahman
Location
Poster 157
Session Format
Poster Presentation
Academic Unit
Department of Mechanical Engineering
Keywords
Allen E. Paulson College of Engineering and Computing Student Research Symposium, Dragonfly Wing
Creative Commons License
This work is licensed under a Creative Commons Attribution 4.0 License.
Presentation Type and Release Option
Presentation (File Not Available for Download)
Start Date
2022 12:00 AM
January 2022
COinS
Jan 1st, 12:00 AM
Finite Element Analysis of a Flapping Dragonfly Wing
Poster 157
• Ornithopter models are not currently feasible for largescale aircraft
• These become more efficient when their size is smaller, making their use for Micro air vehicles very intriguing.
• This research is to determine the stress on a simulated wing for future optimization of a physical model.
