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Volumn 1, Issue , 1998, Pages 489-501
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Effects of modeling refinements on coupled rotor/fuselage vibration analysis
a
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Author keywords
[No Author keywords available]
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Indexed keywords
AERODYNAMIC LOADS;
AIRFRAMES;
COMPUTER SIMULATION;
DATA REDUCTION;
DYNAMIC RESPONSE;
ELASTIC MODULI;
FINITE ELEMENT METHOD;
FUSELAGES;
MATHEMATICAL TRANSFORMATIONS;
MODAL ANALYSIS;
STRUCTURAL ANALYSIS;
VIBRATION CONTROL;
COUPLED NONLINEAR PERIODIC BLADE EQUATIONS;
ELASTIC LINE AIRFRAME MODEL;
FUSELAGE EQUATIONS;
SOFTWARE PACKAGE DAMVIBS;
HELICOPTER ROTORS;
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EID: 0031650244
PISSN: 07334249
EISSN: None
Source Type: Conference Proceeding
DOI: None Document Type: Conference Paper |
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Times cited : (3)
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References (23)
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