Application of Store Separation Wind Tunnel Test Technique into CFD

Author(s):  
Chang-Hyeon Son ◽  
Sang-Hun Kim ◽  
Heekyu Woo
Sensors ◽  
2020 ◽  
Vol 20 (16) ◽  
pp. 4633
Author(s):  
Zengshun Chen ◽  
Yemeng Xu ◽  
Hailin Huang ◽  
Kam Tim Tse

Wind tunnel tests have become one of the most effective ways to evaluate aerodynamics and aeroelasticity in bluff bodies. This paper has firstly overviewed the development of conventional wind tunnel test techniques, including high frequency base balance technique, static synchronous multi-pressure sensing system test technique and aeroelastic test, and summarized their advantages and shortcomings. Subsequently, two advanced test approaches, a forced vibration test technique and hybrid aeroelastic- force balance wind tunnel test technique have been comprehensively reviewed. Then the characteristics and calculation procedure of the conventional and advanced wind tunnel test techniques were discussed and summarized. The results indicated that the conventional wind tunnel test techniques ignored the effect of structural oscillation on the measured aerodynamics as the test model is rigid. A forced vibration test can include that effect. Unfortunately, a test model in a forced vibration test cannot respond like a structure in the real world; it only includes the effect of structural oscillation on the surrounding flow and cannot consider the feedback from the surrounding flow to the oscillation test model. A hybrid aeroelastic-pressure/force balance test technique that can observe unsteady aerodynamics of a test model during its aeroelastic oscillation completely takes the effect of structural oscillation into consideration and is, therefore, effective in evaluation of aerodynamics and aeroelasticity in bluff bodies. This paper has not only advanced our understanding for aerodynamics and aeroelasticity in bluff bodies, but also provided a new perspective for advanced wind tunnel test techniques that can be used for fundamental studies and engineering applications.


2007 ◽  
Vol 2007.82 (0) ◽  
pp. _10-30_
Author(s):  
Ken-taro NAKAGAWA ◽  
Ryo NOMURA ◽  
Hideki KAWAMOTO ◽  
Kazuto NAKAI ◽  
Hirofumi YAMAMORI

2019 ◽  
Vol 11 (5) ◽  
pp. 168781401985306 ◽  
Author(s):  
Fei Xue ◽  
Han Qin ◽  
Yuchao Wang ◽  
Zenghui Jiang ◽  
Xin Jin ◽  
...  

2014 ◽  
Vol 574 ◽  
pp. 480-484
Author(s):  
Jian Zhong Chen ◽  
Pei Qing Liu

In order to study the test technique for the hinge moment of a grid fin in wind tunnel, a platform based on half model support technique was established in FL-23 and FL-31 wind tunnel in China Aerodynamics Research & Development Center (CARDC). The platform developed a wind tunnel test balance, rudder control system and the aerodynamics measurement system. This test technique was important to optimize aerodynamic configurations of a grid fin, design or evaluate the capability of the rudder control system. Nomenclature


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