| タイトル | Computation of turbulent incompressible wing-body junction flow |
| 著者（英） | Burke, R. W. |
| 著者所属（英） | Lockheed Missiles and Space Co. |
| 発行日 | 1989-01-01 |
| 言語 | eng |
| 内容記述 | A three-dimensional incompressible Reynolds-averaged Navier-Stokes solver is presently used in conjunction with a mixing-length turbulence model to characterize the flow around a wing that is mounted on a flat plate, in a wind tunnel, as well as the flow around a support strut within a turnaround duct. Good agreement is found between predicted and observed values of flat-plate static pressure, horseshoe vortex system size, and mean flow velocities in the case of the wing; the case of the strut in a duct is noted to exhibit many of the same overall flow features as the wing/plate. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 89A25236
AIAA PAPER 89-0279 |
| 権利 | Copyright |
|
