All Stories

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