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Method for real-time estimation of aeroelastic flutter using the parametric flutter margin
TS-062490 — An exemplary parametric flutter margin method and associated system that can be used to identify the structural dynamic characteristics of an Unmanned Aerial Vehicle’s wing in a series of Ground Vibration Tests (GVTs) and initial flight-testing study.
The Need
In the aerospace industry, ensuring the safety and certification of aircraft is of paramount importance. One critical challenge faced during the certification process is aeroelastic flutter, an unstable phenomenon that can lead to catastrophic consequences. Conventional flight-testing meth…
- College: College of Engineering (COE)
- Inventors: McCrink, Matthew
- Licensing Officer: Randhawa, Davinder
