| タイトル | Time-marching transonic flutter solutions including angle-of-attack effects |
| 本文（外部サイト） | http://hdl.handle.net/2060/19820015322 |
| 著者（英） | Whitlow, W., Jr.; Seidel, D. A.; Edwards, J. W.; Bennett, R. M. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1982-04-01 |
| 言語 | eng |
| 内容記述 | Transonic aeroelastic solutions based upon the transonic small perturbation potential equation were studied. Time-marching transient solutions of plunging and pitching airfoils were analyzed using a complex exponential modal identification technique, and seven alternative integration techniques for the structural equations were evaluated. The HYTRAN2 code was used to determine transonic flutter boundaries versus Mach number and angle-of-attack for NACA 64A010 and MBB A-3 airfoils. In the code, a monotone differencing method, which eliminates leading edge expansion shocks, is used to solve the potential equation. When the effect of static pitching moment upon the angle-of-attack is included, the MBB A-3 airfoil can have multiple flutter speeds at a given Mach number. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 82N23196
NAS 1.15:83295
AIAA PAPER 82-0685
NASA-TM-83295 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/166148 |
