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A Parallel Multigrid Conservative Patched/Sliding Mesh Algorithm for Turbulent Flow Computation of 3D Complex Aircraft Configurations

Author(s):
Publication title:
AIAA paper
Title of ser.:
AIAA Paper : Aerospace Sciences Meeting and Exhibit
Ser. no.:
2001
Pub. Year:
2001
No.:
2001-1006
Paper no.:
AIAA-2001-1006
Page(from):
1
Page(to):
11
Pages:
11
Pub. info.:
American Institute of Aeronautics and Astronautics
ISSN:
01463705
Language:
English
Call no.:
A07400
Type:
Technical Paper

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