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Volumn 47, Issue 2, 2002, Pages 123-133
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Vibratory loads reduction testing of the NASA/Army/MIT active twist rotor
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Author keywords
[No Author keywords available]
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Indexed keywords
AERODYNAMICS;
PIEZOELECTRICITY;
PRODUCT DESIGN;
TURBOMACHINE BLADES;
VIBRATION CONTROL;
WIND TUNNELS;
VIBRATORY LOADS;
HELICOPTER ROTORS;
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EID: 0036538117
PISSN: 00028711
EISSN: None
Source Type: Journal
DOI: 10.4050/jahs.47.123 Document Type: Article |
Times cited : (102)
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References (22)
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