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Volumn 1, Issue , 1995, Pages 601-612
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Helicopter vibration reduction with trailing edge flaps
a a |
Author keywords
[No Author keywords available]
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Indexed keywords
AERODYNAMIC LOADS;
BENDING (DEFORMATION);
CORRELATION METHODS;
DEFLECTION (STRUCTURES);
DYNAMIC RESPONSE;
MATHEMATICAL MODELS;
STIFFNESS;
TORSIONAL STRESS;
VIBRATION CONTROL;
MAIN ROTOR BLADES;
OPEN LOOP FLAP DEFLECTIONS;
TRAILING EDGE FLAPS;
HELICOPTER ROTORS;
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EID: 0029212635
PISSN: 02734508
EISSN: None
Source Type: Conference Proceeding
DOI: 10.2514/6.1995-1227 Document Type: Conference Paper |
Times cited : (47)
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References (26)
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