Flow simulation of NAL experimental supersonic airplane/booster separation using overset unstructured grids-Reference-Cited by-同舟云学术

Flow simulation of NAL experimental supersonic airplane/booster separation using overset unstructured grids

Published:2001-07 Issue:6 Volume:30 Page:673-688
ISSN:0045-7930
Container-title:Computers & Fluids
language:en
Short-container-title:Computers & Fluids

Author:

Togashi Fumiya,Nakahashi Kazuhiro,Ito Yasushi,Iwamiya Toshiyuki,Shimbo Yuichi

Publisher

Elsevier BV

Subject

General Engineering,General Computer Science

Reference10 articles.

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3. Benek JA, Buning PG, Steger JL. A 3-D chimera grid embedding technique. AIAA Paper 85-1523, 1985

4. Nakahashi K, Togashi F, Sharov D. An intergrid-boundary definition method for overset unstructured grid approach. AIAA Paper 99-3304, June 1999; AIAA J, submitted for publication

5. Obayashi S, Guruswamy GP. Convergence acceleration of an aeroelastic Navier–Stokes solver. AIAA Paper 94-2268, 1994

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