GrabCAD 模型信息
Configurable Test Section Design for Transonic Wind Tunnel · 模型 236768
In this study, a configurable test section designed for transonic wind tunnels. By the design test section can be efficiently and rapidly reconfigured by multiple test teams so that facility utilization can be maximized. In the design, the floor part of the test section is separated from the section. The created space has been modified in a way that allows different test units to be attached to this point, allowing a quick transition to the test phase. A gap was also created where the data and power cables would pass through the floor and reach the control room so that the flow would not be disturbed and test results would not be affected. Design, modeling and assembly were done in computer environment using Dassault Systèmes CATIA (v5 R21) software. Detailed description is in "description pdf" folder.
- 格式
- Rendering、STEP / IGES
- 分类
- Aerospace、Aviation、Industrial design
- 标签
- nasawindtunnelchallenge、transonic、test section、wind tunnel
- 数据更新
- 2026-08-27T03:26:19Z