| タイトル | Computing Flutter Boundaries |
| 著者（英） | Kaza, Krishna Rao V.; Kielb, Robert E. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1989-04-01 |
| 言語 | eng |
| 内容記述 | MISER2 computer program calculates flutter boundaries and aeroelastic response of cascade of arbitrarily mistuned airfoils. Based on typical section formulation incorporating incompressible, subsonic and supersonic cascade, unsteady aerodynamic theories. Each blade modeled as two-degree-of-freedom oscillator that has inertial coupling between bending and torsional motions. Written in FORTRAN 4. |
| NASA分類 | MECHANICS |
| レポートNO | 89B10187
LEW-14380 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/368275 |
