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Volumn 2, Issue , 1995, Pages 937-956
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Structural optimization, for vibration reduction, of composite helicopter rotor blades with advanced geometry tips subject to multidisciplinary constraints
a
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Author keywords
[No Author keywords available]
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Indexed keywords
AERODYNAMIC LOADS;
COMPOUND HELICOPTERS;
CONSTRAINT THEORY;
FINITE ELEMENT METHOD;
FLIGHT DYNAMICS;
MATHEMATICAL MODELS;
OPTIMIZATION;
STABILITY;
STRUCTURAL ANALYSIS;
TURBOMACHINE BLADES;
VIBRATION CONTROL;
AEROELASTIC STABILITY CONSTRAINTS;
COMPOSITE HELICOPTER ROTOR BLADES;
VIBRATORY HUB LOADS;
HELICOPTER ROTORS;
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EID: 0029454912
PISSN: 07334249
EISSN: None
Source Type: Conference Proceeding
DOI: None Document Type: Conference Paper |
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Times cited : (9)
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References (37)
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