| タイトル | Aerodynamic preliminary analysis system 2. Part 1: Theory |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810012500 |
| 著者（英） | Clever, W.; Dunn, K.; Bonner, E. |
| 著者所属（英） | Rockwell International Corp. |
| 発行日 | 1981-04-01 |
| 言語 | eng |
| 内容記述 | A subsonic/supersonic/hypersonic aerodynamic analysis was developed by integrating the Aerodynamic Preliminary Analysis System (APAS), and the inviscid force calculation modules of the Hypersonic Arbitrary Body Program. APAS analysis was extended for nonlinear vortex forces using a generalization of the Polhamus analogy. The interactive system provides appropriate aerodynamic models for a single input geometry data base and has a run/output format similar to a wind tunnel test program. The user's manual was organized to cover the principle system activities of a typical application, geometric input/editing, aerodynamic evaluation, and post analysis review/display. Sample sessions are included to illustrate the specific task involved and are followed by a comprehensive command/subcommand dictionary used to operate the system. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 81N21029
NA-80-374-PT-1
NASA-CR-165627 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/169581 |
