タイトル | Viscous transonic flow computation over Space Shuttle configuration |
著者(英) | Fujii, K.; Kutler, P. |
著者所属(英) | National Aerospace Lab.|NASA Ames Research Center |
発行日 | 1984-01-01 |
言語 | eng |
内容記述 | A thin-layer Navier-Stokes code capable of predicting steady-state viscous flows is applied to the transonic flow over a Space Shuttle configuration. The code is written in the generalized coordinate system, and the grid-generation code of Fujii (1983) is used for the discretization of the flow field. The flow-field computation is done using the CRAY 1S computer at NASA Ames. The computed result is physically reasonable, even though no experimental data is available for the comparison purpose. |
NASA分類 | AERODYNAMICS |
レポートNO | 87A18257 |
権利 | Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/380916 |
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