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Shock and Vibration
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Shock and Vibration
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2015
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Article
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Tab 1
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Research Article
Aeroservoelastic Pitch Control of Stall-Induced Flap/Lag Flutter of Wind Turbine Blade Section
Table 1
Rules for
.
E
ā
ED
1
0.85
0.65
0.5
0.5
0.85
0.85
0.65
0.5
0.5
0.85
0.65
0.5
0.35
0.15
0.65
0.5
0.35
0.35
0.15
0.65
0.5
0.35
0.15
0.15