Design of Subsonic Velocity and Airflow Temperature Controlled Wind Tunnel Test-bed

被引：0

作者：

Li Y. ^{[1
]}

Li G. ^{[2
]}

Wang W. ^{[1
]}

Zhao C. ^{[1
]}

机构：

[1] AVIC Aerodynamics Research Institute, Shenyang

[2] Aviation Engine Academy, Shenyang Aerospace University, Shenyang

来源：

Zhongguo Jixie Gongcheng/China Mechanical Engineering | 2019年 / 30卷 / 12期

关键词：

Heat transfer; Simulation calculation; Temperature control; Wind tunnel design;

D O I：

10.3969/j.issn.1004-132X.2019.12.009

中图分类号：

学科分类号：

摘要：

A minitype opening high speed wind tunnel the test-bed was designed and researched, which was used to be as airflow simulation. The airflow temperature of wind tunnel might be controlled. On the basis of aerodynamics calefaction project design calculation, the software Fluent was adopted to optimize design parameters and the simulation of the flow fields in the test section was carried out. The calculation results of flow and temperature fields indicate that the wind tunnel test-bed design is right. Based on the optimizing design parameters, a high speed wind tunnel was made. Fact measurement indicates that the quality of wind tunnel flow fileds is well, and the test sect temperature accords with the design requests. © 2019, China Mechanical Engineering Magazine Office. All right reserved.

引用

页码：1441 / 1445

页数：4

共 7 条

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