Aerodynamic Damping
Aerodynamic Damping
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Constant speed turbines<br />
Van der Tempel<br />
• Changes in rotor thrust<br />
ξ<br />
aero<br />
T′<br />
1<br />
= ⋅<br />
dV 2 M ω<br />
d<br />
0<br />
n
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