Computational strategies for reliability-based structural optimization of aeroelastic limit cycle oscillations

Structural and Multidisciplinary Optimization

Volumn 45, Issue 1, 2012, Pages 83-99

  Stanford, Bret ^a   Beran, Philip ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

Limit cycle; RBDO; Reduced order modeling

Indexed keywords

ADJOINT METHODS; ADJOINTS; ANALYTICAL GRADIENTS; CANTILEVERED WINGS; COMPUTATIONAL COSTS; COMPUTATIONAL STRATEGY; DESIGN-RELIABILITY; DETERMINISTIC DESIGN; FAILURE PROBABILITY; FIRST ORDER RELIABILITY METHODS; FLOW UNCERTAINTY; FLUTTER POINTS; GRADIENT-BASED OPTIMIZATION; LARGE SYSTEM; LIMIT CYCLE; LIMIT CYCLE OSCILLATION (LCO); MOST PROBABLE POINT; OPTIMAL THICKNESS; PISTON THEORY; PROPER ORTHOGONAL DECOMPOSITIONS; RBDO; REDUCED BASIS; REDUCED-ORDER MODELING; RELIABILITY BASED DESIGN; RELIABILITY DESIGN; REVERSE-TIME INTEGRATION; SAMPLING-BASED; SPECTRAL ELEMENT; UNSTEADY AEROELASTIC SYSTEM;

AEROELASTICITY; DESIGN; FIGHTER AIRCRAFT; PRINCIPAL COMPONENT ANALYSIS; STRUCTURAL OPTIMIZATION;

RELIABILITY;

EID: 84859576546     PISSN: 1615147X     EISSN: 16151488     Source Type: Journal    
DOI: 10.1007/s00158-011-0663-6     Document Type: Article

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