- American Institute of Aeronautics and Astronautics Multi-Dimensional Spectral Difference Method
- AIAA-2003-0880 High-Order Spectral Volume Method for
- AIAA-99-3300 American Institute of Aeronautics and Astronautics
- American Institute of Aeronautics and Astronautics Meshfree Euler Solver using local Radial Basis Functions for
- Spectral (finite) volume method for conservation laws on unstructured grids IV: extension to
- American Institute of Aeronautics and Astronautics Implicit Large Eddy Simulation of Transitional Flow over a SD7003
- American Institute of Aeronautics and Astronautics Efficient Solution Techniques for High-Order Methods on
- American Institute of Aeronautics and Astronautics Knowledge Based Airfoil Aerodynamic and Aeroacoustic
- American Institute of Aeronautics and Astronautics Large Eddy Simulation of Flow over a Cylinder
- Partition Design and Optimization for High-Order Spectral Volume Schemes
- Journal of Computational Physics 174, 381404 (2001) doi:10.1006/jcph.2001.6918, available online at http://www.idealibrary.com on
- Problem C3.4. Heaving and Pitching Airfoil in Wake This problem is aimed at testing the accuracy and performance of high-order flow solvers for
- American Institute of Aeronautics and Astronautics A Frequency-optimized Discontinuous Formulation for
- Relaxation Techniques for High-Order Discretizations of Steady Compressible Inviscid Flows
- American Institute of Aeronautics and Astronautics An Overset Adaptive Cartesian/Prism Grid Method for
- American Institute of Aeronautics and Astronautics Development of High-Order Realizable Finite-Volume
- AIAA 2001-2538 COMPLEX "DIRTY" GEOMETRY HANDLING
- American Institute of Aeronautics and Astronautics A BLOCK LU-SGS IMPLICIT DUAL TIME-STEPPING ALGORITHM
- Problem C1.6. Vortex transport by uniform flow This problem is aimed at testing a high-order method's capability to preserve vorticity in an unsteady
- AIAA JOURNAL Vol. 40, No. 10, October 2002
- International Conference on Multiphase Flow, ICMF 2010, Tampa, FL, May 30 June 4, 2010
- American Institute of Aeronautics and Astronautics Performance of Low-Dissipation Euler Fluxes and
- American Institute of Aeronautics and Astronautics Paper 2010-0720 Partition Design and Optimization for High-Order
- American Institute of Aeronautics and Astronautics A Parameter-Free Generalized Moment Limiter for High-
- INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS Int. J. Numer. Meth. Fluids 2002; 39:703717 (DOI: 10.1002/ d.344)
- American Institute of Aeronautics and Astronautics Simulation of CAA Benchmark Problems Using High-Order
- American Institute of Aeronautics and Astronautics A Fast Level Set Method with Particle Correction on
- American Institute of Aeronautics and Astronautics A Residual-Based Procedure for hp-Adaptation on 2D
- Efficient Implicit Non-linear LU-SGS Approach for Viscous Flow Computation Using High-Order Spectral Difference Method
- An Implicit Space-Time Spectral Difference Method for Discontinuity Capturing Using Adaptive Polynomials
- American Institute of Aeronautics and Astronautics A Study of Viscous Flux Formulations for an Implicit P-
- American Institute of Aeronautics and Astronautics Numerical Simulation of Effects of Buoyancy on Wake
- von KARMAN INSTITUTE FOR FLUID DYNAMICS
- American Institute of Aeronautics and Astronautics Computational Study of Unsteady Flows around Dragonfly
- 0885-7474/04/0200-0137/0 2003 Plenum Publishing Corporation Journal of Scientific Computing, Vol. 20, No. 1, February 2004 ( 2003)
- Journal of Computational Physics 178, 210251 (2002) doi:10.1006/jcph.2002.7041, available online at http://www.idealibrary.com on
- Journal of Computational Physics 179, 665697 (2002) doi:10.1006/jcph.2002.7082
- An Automated, Adaptive, Unstructured, Cartesian-Prism-Based Technique for Moving-Boundary
- American Institute of Aeronautics and Astronautics Effects of Surface Roughness on Laminar Separation Bubble over a
- American Institute of Aeronautics and Astronautics A high order Spectral Volume method for moving boundary
- American Institute of Aeronautics and Astronautics A Numerical Study of Vortex-Dominated Flow around an Oscillating
- American Institute of Aeronautics and Astronautics A High-order Lifting Collocation Penalty Formulation for the
- American Institute of Aeronautics and Astronautics Improvements in the Reliability and Efficiency of
- American Institute of Aeronautics and Astronautics High-Order Adaptive Quadrature-Free Spectral Volume
- Efficient Quadrature-Free 3D High-Order Spectral Volume Method on Unstructured Grids
- American Institute of Aeronautics and Astronautics High Fidelity Multidisciplinary Tool Development for
- American Institute of Aeronautics and Astronautics Efficient Implicit LU-SGS Algorithm for High-Order Spectral
- American Institute of Aeronautics and Astronautics High-Order Multidomain Spectral Difference Method for
- Aerospace Sciences Meeting and Exhibit AIAA 2006-0025 January 9-12, 2006, Reno, Nevada
- American Institute of Aeronautics and Astronautics The Spectral Difference Method for the 2D Euler Equations
- For permission to copy or to republish, contact the copyright owner named on the first page. For AIAA-held copyright, write to AIAA Permissions Department,
- Discontinuous Spectral Difference Method for Conservation Laws on Unstructured Grids
- INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS Int. J. Numer. Meth. Fluids 2004; 45:819838 (DOI: 10.1002/ d.726)
- 1 Copyright 2004 by ASME Proceedings of HTFED2004
- American Institute of Aeronautics and Astronautics Direct Simulation of Surface Roughness Effects with RANS
- American Institute of Aeronautics and Astronautics High-Order Spectral Volume Method for the Navier-Stokes
- AIAA-2004-0082 The Level Set Method on Adaptive Cartesian
- American Institute of Aeronautics and Astronautics EVALUATION OF DISCONTINUOUS GALERKIN AND SPECTRAL VOLUME MEDTHODS
- AIAA-2003-0253 Evaluation of Discontinuous Galerkin and
- Associate Professor, Member AIAA, zjw@egr.msu.edu Project Engineer, Member AIAA, rc171@daimlerchrysler.com
- AIAA 2000-0395 American Institute of Aeronautics and Astronautics
- Gmsh Reference Manual The documentation for Gmsh 2.5
- American Institute of Aeronautics and Astronautics Aerodynamic Performance of a Corrugated Dragonfly Airfoil
- AIAA-2002-1058 American Institute of Aeronautics and Astronautics
- AIAA-2002-0966 American Institute of Aeronautic and Astronautics
- American Institute of Aeronautics and Astronautics A High-Order Unifying Discontinuous Formulation for 3D
- American Institute of Aeronautics and Astronautics A p-Multigrid Spectral Difference Method with Explicit
- Computer Physics Communications 148 (2002) 1729 www.elsevier.com/locate/cpc
- American Institute of Aeronautics and Astronautics Efficient Implementation of High-Order Spectral Volume
- Problem C1.2. Ringleb Problem This problem tests the spatial accuracy of high-order methods. The flow is transonic and smooth.
- Problem C3.5 Direct Numerical Simulation of the Taylor-Green Vortex at Re = 1600
- Department of Aerospace Engineering Iowa State University
- A Comparison of Higher-Order Methods on a Set of Canonical Aerodynamics Applications
- Problem C1.4 Laminar Boundary Layer on a Flat Plate
- 1st International Workshop on HighOrder CFD Methods Sponsored by Fluid Dynamics TC, AFOSR and DLR
- American Institute of Aeronautics and Astronautics A PNPM-CPR Framework for Hyperbolic Conservation Laws
- American Institute of Aeronautics and Astronautics A Low-Frequency Instability/Oscillation near the Airfoil
- 1st International Workshop on High-Order CFD Methods Sponsored by Fluid Dynamics TC, AFOSR and DLR
