GrabCAD 模型信息
Omar 4 Element Airfoil design · 模型 236314
the Omar four-element airfoil, which was tested in a Boeing research wind tunnel in the 1970s [9]. Several configurations ranging from one element to five elements have been tested at Re = 2.83 million and M = 0.201. The double-slotted flap with a slat configuration discussed here is termed model C. The deflection angles of the slat, the first flap, and the second flap are 50° , 0° , and 16.1° , respectively. Three meshes are applied to study the grid convergence, namely, a coarse mesh, medium mesh, and fine mesh, and the numbers of12 grids in these meshes are approximately 7 × 104, 1.4 × 105, and 2.5 × 105, respectively. A schematic diagram of the medium grid
- 格式
- Rendering、SOLIDWORKS
- 分类
- Aerospace、Aviation、Components
- 标签
- devices、high lift、highliftdevices、slats、flaps、wing、2dairfoil、design、solidworks、naca、aerofoil、engineering、aeronautical、aerospace、airfoil
- 数据更新
- 2026-11-03T03:45:03Z
