Complete list of talks from session: Role of HPC in Aerospace Engineering; AIAA Aerospace Meeting, Reno NV, Jan 7-10, 2008
Adjoint-Based Sensitivity Analysis for Computational Fluid Dynamics
 
 
 
 
 
 
Idaho National Laboratory, May 20, 2008 (25Mb pdf).
 
 
 
Unstructured Grid Technology for CFD: Flow Solver Perspectives
 
 
 
 
 
 
Unstructured Grid Technology for CFD
State-of-the-art, State-of-the-practice and Future Directions,
 
 
 
 
 
 
March 26-27, 2008
REEF Conference Center, Eglin, FL
 
 
 
 
 
 
Organized By: CFD Functional Area, PET Program DoD, HPCMP, UAB (4 Mbyte pdf)
 
 
 
High-Order Spatial and Temporal Methods for Simulation and Sensitivity Analysis of
High-SPeed Flows
 
 
 
 
 
 
NASA Hypersonics Program review San Antonio TX, January 23 3008 (14Mb pdf).
 
 
 
Some Long Term Experiences in HPC Programming for CFD Problems
 
 
 
 
 
 
Symposium on Turbulence and Dynamos at Petaspeed, NCAR Boulder CO, October 2007 (5 Mbytes ppt).
 
 
 
Error Estimation and Control for Unsteady Flow Problems with Dynamic Meshes using a Discrete Adjoint Approach
 
 
 
 
 
 
ACE Workshop at North Carolina State University, NCSU, September 2007 (4 Mbytes ppt).
 
 
 
Petaflops Opportunities for the NASA Fundamental Aeronautics Program
 
 
 
 
 
 
Invited talk delivered at 18th AIAA CFD Conference, Miami FL, June 2007 (11 Mbytes pdf).
 
 
 
Unstructured Mesh Discretizations and Solvers for Computational Aerodynamics
 
 
 
 
 
 
Invited talk delivered at 18th AIAA CFD Conference, Miami FL, June 2007 (5 Mbytes ppt).
 
 
 
Results from the 3rd Drag Prediction Workshop using the NSU3D Unstructured Mesh Solver
 
 
 
 
 
 
Talk delivered at AIAA Aerospace Sciences Meeting, Reno NV, Jan 2007 (2 Mbytes ppt).
 
 
 
A Discrete Adjoint-Based Approach for Optimization Problems on Three-Dimensional Unstructured Meshes AIAA talk, Reno NV, Jan 2006.(430K ppt)
 
 
 
Progress in Unstructured Mesh Techniques (Talk presented Boeing Commercial Aircraft
Seattle, Nov 18, 2005 (6Mbyte ppt)
 
 
 
 
 
 
High Resolution Aerospace Applications on the NASA Columbia Supercomputer (Talk presented at SC05, Seattle, Nov 17, 2005 (7Mbyte ppt)
 
 
 
 
 
 
Grid Resolution Study of a Drag Prediction Workshop Configuration using the NSU3D Unstructured Mesh Solver (23rd AIAA Applied Aerodynamics Conference, Toronto, CA, June 2005)
 
 
 
 
 
 
Presentation for workshop at Stanford Universitry in Honor of Prof. A. Jameson's 70th birthday
 
 
 
 
 
 
Drag Prediction using NSU3D (Presentation for the 2nd AIAA Drag Prediction Workshop, June 2003 (665K ppt)
 
 
 
 
 
 
Revisiting the Least-Squares Gradient Procedure for Gradient Construction on Unstructured Meshes (665K ppt)
 
 
 
 
 
 
AIAA paper 2003-3986, presented at the AIAA CFD conference, Orlando, FL, June 2003.
 
 
 
Computational Aerodynamics Using Unstructured Meshes (4.5 Mb ppt)
 
 
 
 
 
 
National Institute of Aerospace (NIA) Informal Seminar, NIA Headquarters, Hampton, VA, March 21, 2003.
 
 
 
 
 
 
(See archived webcast at : http://nasatechnology.nasa.gov)
 
 
 
Drag Prediction using Unstructured Mesh Solvers (9.5 Mb ppt)
 
 
 
 
 
 
VKI Lecture on Drag Prediction, Von Karman Institute for Fluid Dynamics, Rhode St Genese, Belgium, Feb 3-7th, 2003.
Drag Prediction using Unstructured Mesh Solvers (10.0 Mb pdf)
 
 
 
 
 
 
VKI Lecture Notes for above presentation, Feb 3-7th, 2003.
Unstructured Mesh Related Issues in CFD-based Analysis and Design (5.5 Mb ppt)
 
 
 
 
 
 
Invited talk delivered at the 11th International Meshing Roundtable, Ithaca NY, Sept 17th, 2002.
The Development of Unstructured Grid Methods for Computational Aerodynamics (4.2 Mb ppt)
 
 
 
 
 
 
talk delivered in the Depart. of Mech and Aerospace Engineering, Cornell University, Ithaca NY, Sept 17th, 2002.
The Development of Unstructured Grid Methods for Computational Aerodynamics (3.8Mb pdf)
 
 
 
 
 
 
talk delivered at University of Illinois at Urbana-Champaign, April 29th, 2002
Transonic Drag Prediction using an Unstructured Multigrid Solver (4Mb pdf)
 
 
 
 
 
 
(a summary of the final results from the AIAA Drag predicion workshop using NSU3D)
 
 
 
 
 
 
talk delivered at 40th AIAA Aerospace Sciences Meeting, Reno NV, Jan 2002.