| タイトル | User's Guide for a Modular Flutter Analysis Software System (Fast Version 1.0) |
| 本文（外部サイト） | http://hdl.handle.net/2060/19780020158 |
| 著者（英） | Bennett, R. M.; Desmarais, R. N. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1978-05-01 |
| 言語 | eng |
| 内容記述 | The use and operation of a group of computer programs to perform a flutter analysis of a single planar wing are described. This system of programs is called FAST for Flutter Analysis System, and consists of five programs. Each program performs certain portions of a flutter analysis and can be run sequentially as a job step or individually. FAST uses natural vibration modes as input data and performs a conventional V-g type of solution. The unsteady aerodynamics programs in FAST are based on the subsonic kernel function lifting-surface theory although other aerodynamic programs can be used. Application of the programs is illustrated by a sample case of a complete flutter calculation that exercises each program. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 78N28101
NASA-TM-78720 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/178298 |
