| タイトル | Development of an integrated BEM approach for hot fluid structure interaction |
| 本文（外部サイト） | http://hdl.handle.net/2060/19890005743 |
| 著者（英） | Honkala, Keith A.; Banerjee, Prasanta K.; Dargush, Gary F. |
| 著者所属（英） | Calspan-Buffalo Univ. Research Center |
| 発行日 | 1988-12-20 |
| 言語 | eng |
| 内容記述 | In the present work, the boundary element method (BEM) is chosen as the basic analysis tool, principally because the definition of temperature, flux, displacement and traction are very precise on a boundary-based discretization scheme. One fundamental difficulty is, of course, that a BEM formulation requires a considerable amount of analytical work, which is not needed in the other numerical methods. Progress made toward the development of a boundary element formulation for the study of hot fluid-structure interaction in Earth-to-Orbit engine hot section components is reported. The primary thrust of the program to date has been directed quite naturally toward the examination of fluid flow, since boundary element methods for fluids are at a much less developed state. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 89N15114
NASA-CR-184587
NAS 1.26:184587 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/143945 |
