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- 23rd Applied Aerodynamics Conference, June 6-9 2005, Toronto, Canada Grid Resolution Study of a Drag Prediction Workshop
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- Linearization of the Coupled Unsteady Fluid-Structure Equations: Application to Flutter Control
- Efficient Hessian Calculations using Automatic Differentiation and the Adjoint Method
- Implicit Solution of the Unsteady Euler Equations for High-Order Accurate Discontinuous Galerkin
- AIAA 20051268 High-Order Discontinuous Galerkin
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- A Dynamic Sampling Method for Kriging and Cokriging Surrogate Models
- An Overset Unstructured Mesh Discontinuous Galerkin Approach for Aerodynamic Problems
- 49th AIAA Aerospace Sciences Meeting and Exhibit, January 47, 2011, Orlando, FL An hp-Adaptive Discontinuous Galerkin Solver for
- American Institute of Aeronautics and Astronautics Derivative-Enhanced Variable Fidelity Surrogate Modeling
- American Institute of Aeronautics and Astronautics Design Optimization Utilizing
- Spatially Non-Uniform Time-Step Adaptation for Functional Outputs in Unsteady Flow Problems
- Parameter Sensitivity Analysis for Hypersonic Viscous Flow using a Discrete Adjoint Approach
- 48th AIAA Aerospace Sciences Meeting and Exhibit, January 47, 2010, Orlando, FL Efficient Solution Techniques for Discontinuous Galerkin
- Efficient Solution Techniques for Discontinuous Galerkin Discretizations of the Navier-Stokes Equations on Hybrid
- COVER SHEET NOTE: This conversheet is intended for you to list your article title and author(s) name
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- A Mesh Deformation Strategy Optimized by the Adjoint Method on Unstructured meshes
- 44th AIAA Aerospace Sciences Meeting and Exhibit, January 912, 2006, Reno, NV Discontinuous Galerkin Methods Using an hp-Multigrid Solver
- Higher-order Time Integration Schemes for Aeroelastic Applications on Unstructured Meshes
- A Discrete Adjoint-Based Approach for Optimization Problems on Three-Dimensional Unstructured Meshes
- Revisiting the Least-Squares Procedure for Gradient Reconstruction on Unstructured
- AIAA 2002-2734 Higher Order Time Integration
- American Institute of Aeronautics and Astronautics Current Status and Future Prospects for the Numerical
- Efficient Solutions of the Euler Equations in a Time-Adaptive Space-Time Framework
- !"$#%&(') #"0 #"1#"2&435&687
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- Overview of the Helios Version 2.0 Computational Platform for Rotorcraft Simulations
- Prediction of Helicopter Maneuver Loads Using BDF/Time Spectral Method on Unstructured Meshes
- AIAA 20051222 Unstructured Dynamic Meshes with
- Discrete Adjoint Based Time-Step Adaptation and Error Reduction in Unsteady Flow Problems
- Optimization-based Multigrid Applied to Aerodynamic Shape Design
- Adjoint-based h-p Adaptive Discontinuous Galerkin Methods for the Compressible Euler Equations
- A Coupled Unstructured-Adaptive Cartesian CFD Approach for Hover Prediction
- Analysis of "p"-Multigrid for Continuous and Discontinuous Finite Element Discretizations
- Application of the Helios Computational Platform to Rotorcraft Flowfields
- Unsteady Discrete Adjoint Formulation for High-order Discontinuous Galerkin Discretizations in Time-dependent
- Time Spectral Method for Periodic and Quasi-Periodic Unsteady Computations on Unstructured Meshes
- NSU3D Results for the First AIAA High Lift Prediction Workshop
- Unstructured Mesh Discretizations and Solvers for Computational Aerodynamics
- Solution of the Unsteady Discrete Adjoint for Three-Dimensional Problems on Dynamically
- Grid Quality and Resolution Issues from the Drag Prediction Workshop Series
- A Multi-Code Python-Based Infrastructure for Overset CFD with Adaptive Cartesian Grids
- Development of An Adaptive Space-Time Method for High-Order Resolution of Discontinuities
- Results from the 3rd Drag Prediction Workshop Using the NSU3D Unstructured Mesh Solver
- Discrete Adjoint Based Adaptive Error Control in Unsteady Flow Problems
- Capability Enhancements in Version 3 of the Helios High-Fidelity Rotorcraft Simulation Code
- 50th AIAA Aerospace Sciences Meeting and Exhibit, January 9-12, 2012, Nashville, TN Robust Computation of Turbulent flows using a Discontinuous
- Extensions of Time Spectral Methods for Practical Rotorcraft Problems
- Mixed Aleatory/Epistemic Uncertainty Quantification for Hypersonic Flows via Gradient-Based Optimization
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