A stochastic analysis of the limit cycle behavior of a nonlinear aeroelastic model using the response surface method

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

Volumn 4, Issue , 2005, Pages 2318-2338

  Attar, Peter J ^a,c,d   Dowell, Earl H ^b,d,e,f  

^a Computational Sciences Branch ^*  (United States)

^b DUKE UNIVERSITY   (United States)

^c AIR FORCE RESEARCH LABORATORY   (United States)

^d AIAA   (United States)

^e Center for Nonlinear and Complex Systems

^f Duke University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; MATHEMATICAL MODELS; MONTE CARLO METHODS; PARAMETER ESTIMATION; RANDOM PROCESSES; REGRESSION ANALYSIS; STOCHASTIC CONTROL SYSTEMS;

COMPUTATIONAL EFFICIENCY; LIMIT CYCLE; RANDOM INPUT; RESPONSE SURFACE METHOD;

AERODYNAMICS;

EID: 28844486747     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-1986     Document Type: Conference Paper

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