Application of a weighted average surrogate approach to helicopter rotor blade vibration reduction

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 3, Issue , 2007, Pages 2370-2394

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

^a UNIVERSITY OF MICHIGAN   (United States)

^b UNIVERSITY OF FLORIDA   (United States)

^c AIAA   (United States)

^d AHS ^*

Author keywords

[No Author keywords available]

Indexed keywords

HELICOPTER ROTORS; SENSITIVITY ANALYSIS; VIBRATION CONTROL;

MULTIPLE APPROXIMATION METHODS; VIBRATION REDUCTION; WEIGHTED AVERAGE SURROGATE APPROACH;

APPROXIMATION ALGORITHMS;

EID: 34547510555     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-1898     Document Type: Conference Paper

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