| タイトル | Multidisciplinary High-Fidelity Analysis and Optimization of Aerospace Vehicles |
| 本文（外部サイト） | http://hdl.handle.net/2060/19990116394 |
| 著者（英） | Salas, A. O.; Mukhopadhyay, V.; Walsh, J. L.; Barthelemy, J.-F.; Samareh, J. A.; Townsend, J. C. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2000-01-01 |
| 言語 | eng |
| 内容記述 | An objective of the High Performance Computing and Communication Program at the NASA Langley Research Center is to demonstrate multidisciplinary shape and sizing optimization of a complete aerospace vehicle configuration by using high-fidelity, finite element structural analysis and computational fluid dynamics aerodynamic analysis in a distributed, heterogeneous computing environment that includes high performance parallel computing. A software system has been designed and implemented to integrate a set of existing discipline analysis codes, some of them computationally intensive, into a distributed computational environment for the design of a highspeed civil transport configuration. The paper describes the engineering aspects of formulating the optimization by integrating these analysis codes and associated interface codes into the system. The discipline codes are integrated by using the Java programming language and a Common Object Request Broker Architecture (CORBA) compliant software product. A companion paper presents currently available results. |
| NASA分類 | Aircraft Design, Testing and Performance |
| レポートNO | AIAA Paper 2000-0418 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/95673 |
