Analysis and testing of Mach scaled rotor model with piezoelectric bender actuated trailing-edge flaps for helicopter vibration control
Keyword(s):
2006 ◽
Vol 29
(5)
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pp. 1201-1209
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Keyword(s):
Using the Complete Authority of Multiple Active Trailing-edge Flaps for Helicopter Vibration Control
2008 ◽
Vol 14
(8)
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pp. 1175-1199
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2001 ◽
Vol 10
(1)
◽
pp. 1-14
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Keyword(s):
2014 ◽
Vol 47
(9)
◽
pp. 1243-1263
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