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

DOI10.1007/s00158-011-0663-6zbMath1274.74248OpenAlexW2027111954MaRDI QIDQ381694

Philip S. Beran, Bret K. Stanford

Publication date: 15 November 2013

Published in: Structural and Multidisciplinary Optimization (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s00158-011-0663-6

zbMATH Keywords

limit cyclereduced order modelingRBDO

Mathematics Subject Classification ID

Topological structure of integral curves, singular points, limit cycles of ordinary differential equations (34C05) Reliability, availability, maintenance, inspection in operations research (90B25) Compliance or weight optimization in solid mechanics (74P05)

Related Items (2)

Minimum-mass panels under probabilistic aeroelastic flutter constraints ⋮ Uncertainty Quantification in Aeroelasticity

Cites Work

• A review of optimization of structures subjected to transient loads
• Control of limit cycle oscillations of a two-dimensional aeroelastic system
• Reduced-order fluid/structure modeling of a complete aircraft configuration
• Efficient model reduction in nonlinear dynamics using the Karhunen-Loève expansion and dual-weighted-residual methods
• A spectral viscosity method for correcting the long-term behavior of POD models.
• Spectral element method in time for rapidly actuated systems
• Reliability-based shape optimization of structures undergoing fluid--structure interaction phenomena
• A reduced-order cyclic method for computation of limit cycles
• The method of proper orthogonal decomposition for dynamical characterization and order reduction of mechanical systems: an overview
• Uncertainty quantification of limit-cycle oscillations
• Dimensional model reduction in non‐linear finite element dynamics of solids and structures
• A Time Integration Algorithm for Structural Dynamics With Improved Numerical Dissipation: The Generalized-α Method
• Minimal Repetition Dynamic Checkpointing Algorithm for Unsteady Adjoint Calculation
• The method of moving asymptotes—a new method for structural optimization
• Nonlinear stall flutter and divergence analysis of cantilevered graphite/epoxy wings
• Finite element nonlinear panel flutter with arbitrary temperatures in supersonic flow
• On the use of the P–TFE method for panel flutter optimization
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