π Case Study
Coastal Texas Tracker Array Aeroelastic Flutter Event
Sustained flutter observed at 14β18 m/s winds, causing actuator lockups and module delamination
ποΈ Project Overview
350MW coastal site with salt-corroded torque tubes and unshielded exposure
π― Challenge
Sustained flutter observed at 14β18 m/s winds, causing actuator lockups and module delamination
π§ Design Approach
Installed vortex suppression strakes (12 mm height, Ξ»/D = 0.18); replaced corroded tubes with 316SS; added pitch-rate limiting firmware
π Design Diagram
AI-generated project design illustration
π Key Calculations
Strouhal Number Match
St = fΒ·D/V
Result: 0.172 (target), 0.175 (achieved)
Shifted shedding frequency out of resonant band
Critical Flutter Velocity
V_f = ΟΒ·f_nΒ·D/(2Β·StΒ·β(ΟΒ·k))
Result: 12.3 m/s β 22.8 m/s
Raised threshold above 95th-percentile wind speed
π Results
Flutter eliminated; actuator failure rate dropped from 21/yr to 0; 3-year ROI on strake retrofitπ‘ Lessons Learned
- β’Corrosion reduces effective stiffness more than strength β requires dynamic re-evaluation
- β’Pitch-rate limiting must be coordinated with structural DAF to avoid control-induced resonance
β Key Takeaways
- 1Corrosion reduces effective stiffness more than strength β requires dynamic re-evaluation
- 2Pitch-rate limiting must be coordinated with structural DAF to avoid control-induced resonance