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Volumn 3, Issue , 1999, Pages 2275-2289
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Performance enhancement of a composite tilt-rotor using aeroelastic tailoring
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Author keywords
[No Author keywords available]
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Indexed keywords
AIRCRAFT;
CONSTRAINT THEORY;
EQUATIONS OF MOTION;
FINITE ELEMENT METHOD;
MATHEMATICAL MODELS;
OPTIMIZATION;
PERFORMANCE;
ROTORS;
TURBOMACHINE BLADES;
AEROELASTIC TAILORING;
AUTOROTATIONAL INERTIA;
BLADE CROSS SECTIONAL ANALYSIS;
BLADE TWIST;
BOX DIMENSIONS;
COMPOSITE TILT ROTOR;
FINITE STATE DYNAMIC INFLOW THEORY;
OBJECTIVE FUNCTION;
PERFORMANCE ENHANCEMENT;
WALL THICKNESS;
AERODYNAMICS;
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EID: 0032657008
PISSN: 02734508
EISSN: None
Source Type: Conference Proceeding
DOI: None Document Type: Article |
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Times cited : (3)
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References (24)
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