Extension of flutter prediction parameter for multimode flutter systems

Journal of Aircraft

Volumn 42, Issue 1, 2005, Pages 285-288

  Bae, Jae Sung ^a,d,e   Kim, Jong Yun ^b,f   Lee, In ^b,f   Matsuzaki, Yuji ^c,f   Inman, Daniel J ^a,d  

^a VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^b Korea Advanced Institute of Science and Technology (KAIST)   (South Korea)

^c NAGOYA UNIVERSITY   (Japan)

^d Ctr Intelligent Mat Syst/Struct   (United States)

^e Korea Institute of Energy Research (KIER)   (South Korea)

^f Department of Mechanical Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; COMPUTATIONAL METHODS; CURVE FITTING; DATA REDUCTION; FLUTTER (AERODYNAMICS); IDENTIFICATION (CONTROL SYSTEMS); PARAMETER ESTIMATION; REGRESSION ANALYSIS;

AUTOREGRESSIVE MOVING AVERAGE (ARMA) MODEL; CRITICAL SPEED; FLUTTER BOUNDARY; PLATE WINGS;

AERODYNAMICS;

EID: 13844297744     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.6440     Document Type: Article

References (12)

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