Reliability-based design optimization of nonlinear aeroelasticity problems

Journal of Aircraft

Volumn 47, Issue 3, 2010, Pages 992-998

  Missoum, Samy ^a,c   Dribusch, Christoph ^a,c   Beran, Philip ^b,d  

^a UNIVERSITY OF ARIZONA   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c Aerospace and Engineering Mechanics 1 University Station   (United States)

^d Design and Analysis Methods Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTICITY; CONTROL NONLINEARITIES; DEGREES OF FREEDOM (MECHANICS); FLUTTER (AERODYNAMICS); OPTIMIZATION; RELIABILITY; SUPPORT VECTOR MACHINES;

AEROELASTIC CONSTRAINTS; DESIGN VARIABLES; LIMIT CYCLE OSCILLATION (LCO); NON-LINEAR STIFFNESS; NONLINEAR AEROELASTICITY; RELIABILITY-BASED DESIGN OPTIMIZATION; TWO-DEGREE OF FREEDOM;

MACHINE DESIGN;

EID: 77953163372     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.46665     Document Type: Article

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