| タイトル | Steady-State Solution of a Flexible Wing |
| 本文（外部サイト） | http://hdl.handle.net/2060/20010000429 |
| 著者（英） | Chandra, Suresh; Karkehabadi, Reza; Krishnamurthy, Ramesh |
| 著者所属（英） | North Carolina Agricultural and Technical State Univ. |
| 発行日 | 1997-02-01 |
| 言語 | eng |
| 内容記述 | A fluid-structure interaction code, ENSAERO, has been used to compute the aerodynamic loads on a swept-tapered wing. The code has the capability of using Euler or Navier-Stokes equations. Both options have been used and compared in the present paper. In the calculation of the steady-state solution, we are interested in knowing how the flexibility of the wing influences the lift coefficients. If the results of a flexible wing are not affected by the flexibility of the wing significantly, one could consider the wing to be rigid and reduce the problem from fluid-structure interaction to a fluid problem. |
| NASA分類 | Aerodynamics |
| レポートNO | URC97070 |
| 権利 | No Copyright |
|
