All Stories

  1. Assessment of Projection-Based Model Order Reduction for a Benchmark Hypersonic Flow Problem
  2. Enabling digital twinning via a modeling method leveraging experimental and numerical data
  3. Active Manifold and Model Reduction for Multidisciplinary Analysis and Optimization
  4. Training a Neural-Network-Based Surrogate Model for Aerodynamic Optimization Using a Gaussian Process
  5. Feasible Probabilistic Learning Method for Model-Form Uncertainty Quantification in Vibration Analysis
  6. Effects of Structural Parameters on the FSI Simulation of Supersonic Parachute Deployments
  7. Towards a Validated FSI Computational Framework for Supersonic Parachute Deployments
  8. Studies into Computational Modeling of Fabric in Inflatable Structures
  9. Parameterization Framework for the MDAO of Wing Structural Layouts
  10. A Stochastic Projection-Based Hyperreduced Order Model for Model-Form Uncertainties in Vibration Analysis
  11. Modeling and Quantification of Model-Form Uncertainties in Eigenvalue Computations Using a Stochastic Reduced Model
  12. Accelerated mesh sampling for the hyper reduction of nonlinear computational models
  13. Scalable Environment for Quantification of Uncertainty and Optimization in Industrial Applications (SEQUOIA)
  14. A nonparametric probabilistic approach for quantifying uncertainties in low-dimensional and high-dimensional nonlinear models
  15. Gradient based aerodynamic shape optimization using the FIVER embedded boundary method
  16. A High-order Discontinuous Galerkin Method for Unsteady Flow Problems
  17. On the Use of Discrete Nonlinear Reduced-Order Models for the Prediction of Steady-State Flows Past Parametrically Deformed Complex Geometries
  18. Parameterization Framework for Aeroelastic Design Optimization of Bio-Inspired Wing Structural Layout
  19. Enforcing Boundary Conditions for Discrete Nonlinear Aerodynamic Reduced-Order Models
  20. Nonlinear Aeroelastic Analysis of Highly Flexible Flapping Wings Using an ALE Formulation of Embedded Boundary Method