Multiple-surrogate approach to helicopter rotor blade vibration reduction

AIAA Journal

Volumn 47, Issue 1, 2009, Pages 271-282

  Glaz, Bryan ^a,c   Goel, Tushar ^b,c,d   Liu, Li ^a,c   Friedmann, Peretz P ^a,c   Haftka, Raphael T ^b,c  

^a UNIVERSITY OF MICHIGAN   (United States)

^b UNIVERSITY OF FLORIDA   (United States)

^c Department of Aerospace Engineering ^*

^d LIVERMORE SOFTWARE TECHNOLOGY CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; DESIGN; HELICOPTERS; POLYNOMIAL APPROXIMATION; STRUCTURAL MEMBERS; THEOREM PROVING; TURBOMACHINE BLADES;

ADDITIONAL COSTS; APPROXIMATION METHODS; BASELINE DESIGNS; DESIGN VARIABLES; FLIGHT CONDITIONS; HELICOPTER ROTOR BLADES; HELICOPTER VIBRATIONS; MULTIPLE APPROXIMATION METHODS; OBJECTIVE FUNCTIONS; OPTIMIZED DESIGNS; REDUCTION PROBLEMS; ROTOR BLADES; SURROGATE APPROACHES; VIBRATION DESIGNS; VORTEX INTERACTIONS;

HELICOPTER ROTORS;

EID: 58149376081     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.40291     Document Type: Article

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