Parallel Adaptive Finite Element Euler Flow Solver for Rotary Wing Aerodynamics-Reference-Cited by-同舟云学术

Parallel Adaptive Finite Element Euler Flow Solver for Rotary Wing Aerodynamics

Published:1997-06 Issue:6 Volume:35 Page:937-944
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Bottasso Carlo L.¹,Shephard Mark S.¹

Affiliation:

1. Rensselaer Polytechnic Institute, Troy, New York 12180

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.187

Reference20 articles.

1. 1Johan, Z. “ Data Parallel Finite Element Techniques for Large-Scale Computational Fluid Dynamics,” Ph.D. Thesis, Mechanical Engineering Dept.Stanford Univ., Stanford, CA,July 1992.

2. Implementation of implicit finite element methods for incompressible flows on the CM-5

3. Load balancing for the parallel adaptive solution of partial differential equations

4. The design and implementation of a parallel unstructured Euler solver using software primitives

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