Guided and closed annular wind tunnel
A guided, ring-shaped technology, applied in the field of experimental wind tunnels, to achieve the effect of controllability, great stability, and simple structure
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Publication Date
- 2010-12-29
- Estimated Expiration
- Not applicable · inactive patent
Smart Images
Figure 1 Figure 2 Figure 3
Abstract
Description
technical field
[0001] The invention relates to an experimental wind tunnel, in particular to a guided closed annular wind tunnel which can provide various flow velocities, streamlines, flows, etc. for simulating the actual flow field. Background technique
[0002] A wind tunnel is a pipe-shaped experimental device that can artificially generate and control airflow to simulate the flow of air around an aircraft or object, measure the effect of airflow on an object and observe physical phenomena. It is aerodynamic The most commonly used and most effective tool for experimentation. Wind tunnel experiments are an indispensable part of aircraft development. It not only plays an important role in the research and development of aviation and aerospace engineering, but with the development of industrial aerodynamics, it is also more and more widely used in transportation, housing construction, wind energy utilization and environmental protection.
[0003] Wind tunnels are divide...
Examples
Embodiment Construction
[0037] Specific embodiments are given below in conjunction with the accompanying drawings to further illustrate how the present invention is realized.
[0038] like figure 1 , figure 2 , image 3 As shown, the guided closed annular wind tunnel of the present invention includes an annular chamber 1, and the annular chamber 1 is an elliptical pipe structure, which is an elliptical shape formed by connecting two semicircular arcs with two common tangent lines. tube annulus. The tube wall of the annular chamber 1 is provided with a plurality of exhaust ports 7, a plurality of gas injection ports 8 and a plurality of airtight hatches 9; Correspondingly and tangentially arranged on the side walls are multiple pairs of air guide tubes 2 and return air tubes 3 communicating with the annular chamber 1, and the other ends of each pair of air guide tubes 2 and return air tubes 3 are connected to a three-way body 4. A group of power guiding devices 6 is connected between two adjacen...