Technical Paper

Individual Blade Pitch Control (IBC) for Vibration Reduction of Lift-Offset Coaxial Rotor Vehicles with Auxiliary Propulsion

F-0079-2023-18032

5/16/2023

Event
Vertical Flight Society 79th Annual Forum and Technology Display
Authors
Jessica Beyer The Pennsylvania State University
Edward Smith The Pennsylvania State University
Sven Schmitz The Pennsylvania State University
Jianhua Zhang The Pennsylvania State University
Abstract
Content

Meta Tags
Topics
Pitch
Propellers and rotors
Vibration
Affiliated or Co-Author
The Pennsylvania State University
Details
DOI
https://doi.org/10.4050/F-0079-2023-18032
Citation
Beyer, J., Smith, E., Schmitz, S., and Zhang, J., "Individual Blade Pitch Control (IBC) for Vibration Reduction of Lift-Offset Coaxial Rotor Vehicles with Auxiliary Propulsion," Vertical Flight Society 79th Annual Forum and Technology Display, West Palm Beach, Florida, May 16, 2023, https://doi.org/10.4050/F-0079-2023-18032.
Additional Details
Publisher
The Vertical Flight Society
Published
5/16/2023
Product Code
F-0079-2023-18032
Content Type
Technical Paper
Language
English