Performance Comparisons of Parallel Implicit Solvers for Hypersonic Flow Computations on Unstructured Meshes

Performance Comparisons of Parallel Implicit Solvers for Hypersonic Flow Computations on Unstructured Meshes

Author(s):

I. Nompelis ( University of Minnesota, Minneapolis, MN )
T. Wan
G. Candler

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA Computational Fluid Dynamics Conference

Ser. no.:

2007

Pub. Year:

2007

No.:

2007-4334

Paper no.:

AIAA Paper 2007-4334

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200713 [CD-ROM 2007 Disc 13]

Type:

Technical Paper

Details

TDL ID:	ZA00049501
Series ID:	PA00000168
Conf. info. (Name):	AIAA Computational Fluid Dynamics Conference
Conf. info. (Number):	18th
Conf. info. (Venue):	Miami, Florida
Conf. info. (Date):	2007.06.25-2007.06.28

Similar Items:

1 Technical Paper A Parallel Unstructured Implicit Solver for Hypersonic Reacting Flow Simulation Nompelis, I., Drayna, T., Candler, G. American Institute of Aeronautics and Astronautics	7 Technical Paper CFD Validation for Hypersonic Flight: Real Gas Flows. Candler, G.V., Nompelis, I. American Institute of Aeronautics and Astronautics
2 Technical Paper Development of a Hybrid Unstructured Implicit Solver for the Simulation of Reacting Flows Over Complex Geometries Nompelis, I., Drayna, T., Candler, G. American Institute of Aeronautics and Astronautics	8 Technical Paper A Parallel Implicit CFD Code for the Simulation of Ablating Re-Entry Vehicles I. Nompelis, G. Candler, R. Conti American Institute of Aeronautics and Astronautics
3 Technical Paper Development of Stencil-Based Mesh Partitioning for Parallel Unstructured CFD Solvers V. Gidzak, I. Nompelis, G. Candler American Institute of Aeronautics and Astronautics	9 Technical Paper Investigation of Hypersonic Double-Cone Flow Experiments at High Enthalpy in the LENS Facility I. Nompelis, G. Candler American Institute of Aeronautics and Astronautics
4 Technical Paper High Performance Parallel Implicit Computations of Three-dimensional Supersonic Magnetohydrodynamics Using PETSc Library T. Wan, G. Candler American Institute of Aeronautics and Astronautics	10 Technical Paper Hypersonic Inward Turning Inlets: Design and Optimization T. Drayna, I. Nompelis, G. Candler American Institute of Aeronautics and Astronautics
5 Technical Paper Comparison of Physical Models in Computations of High-Enthalpy Double-Cone Flows M. Druguet, G. Candler, I. Nompelis American Institute of Aeronautics and Astronautics	11 Technical Paper Simulations of Viscous Hypersonic Double-Cone Flows: Influence of Numerics Druguet, M., Candler, G., Nompelis, I. American Institute of Aeronautics and Astronautics
6 Technical Paper Computational Investigation of Hypersonic Viscous/Inviscid Interactions in High Enthalpy Flows Nompelis, I., Candler, G.V., Holden, M.S., Wadhams, T.P. American Institute of Aeronautics and Astronautics	12 Technical Paper DSMC-CFD Comparison of a High Altitude, Extreme-Mach Number Reentry Flow T. Ozawa, I. Nompelis, D. Levin, M. Barnhardt, G. Candler American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12