Flight Testing of Automated Rotor Track and Balance using Active Trim Tab and Pitch Control Rod Technologies

F-0079-2023-18040

5/16/2023

Authors
Abstract
Content

Meta TagsDetails
Pages
13
Citation
Vanacore, R., DiOttavio, J., Reilly, P., and Bates, P., "Flight Testing of Automated Rotor Track and Balance using Active Trim Tab and Pitch Control Rod Technologies," Vertical Flight Society 79th Annual Forum and Technology Display, West Palm Beach, Florida, May 16, 2023, .
Additional Details
Publisher
Published
5/16/2023
Product Code
F-0079-2023-18040
Content Type
Technical Paper
Language
English