Flight Testing of Automated Rotor Track and Balance using Active Trim Tab and Pitch Control Rod Technologies
- Presented at Forum 79
- 13 pages
- SKU # : F-0079-2023-18040 Dynamics
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Flight Testing of Automated Rotor Track and Balance using Active Trim Tab and Pitch Control Rod Technologies
Authors / Details:Ray Vanacore, Preston Bates, Sikorsky a Lockheed Martin Company
Jim DiOttavio, DEVCOM AvMC
Patrick Reilly, Beta Technologies
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