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Volumn 1, Issue III, 2000, Pages 1850-1864
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Vibration reduction in rotorcraft using an enhanced ACSR model
a a |
Author keywords
[No Author keywords available]
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Indexed keywords
AERODYNAMICS;
ALGORITHMS;
FINITE ELEMENT METHOD;
FUSELAGES;
VIBRATION CONTROL;
ACTIVE CONTROL OF STRUCTURAL RESPONSE;
COEFFICIENT OF PRESSURE;
ROTORCRAFT;
VIBRATION REDUCTION;
VIBRATORY LOADS;
ROTORS;
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EID: 0033670812
PISSN: 02734508
EISSN: None
Source Type: Conference Proceeding
DOI: 10.2514/6.2000-1687 Document Type: Conference Paper |
Times cited : (5)
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References (26)
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