| タイトル | Panel Flutter Constraints: Analytic Sensitivities and Approximations Including Planform Shape Design Variables |
| 著者（英） | Livne, Eli; Mineau, David |
| 著者所属（英） | Washington Univ. |
| 発行日 | 1997-08-01 |
| 言語 | eng |
| 内容記述 | Analytical sensitivities of panel flutter constraints with respect to panel shape as well as thickness and material properties are derived and numerically tested. Cases of fixed in-plane loads and cases in which in-plane loads are variable (depending on panel and overall wing shape as well as material and sizing design variables) are considered. Accuracy of approximations and range of move limits required are studied in preparation for integration with nonlinear programming/approximation concept aeroelastic design synthesis methodology. |
| NASA分類 | Aircraft Stability and Control |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/344124 |
