发明名称 |
SENSOR TYPE WIND EXPERIMENTAL MODEL SETTING SYSTEM |
摘要 |
The present invention relates to a sensor type wind tunnel test model setting system. The sensor type wind tunnel test model setting system includes: a contactless distance measurement sensor (20) generating a transmitting and receiving signal to detect data on a posture angle (an attack angle, a reentering angle, and a roll angle) of a wind tunnel test model (100) installed in a wind tunnel test space; a signal processing module (30) extracting distance information of the wind tunnel test model (100) from the data on the posture angle of the contactless distance measurement sensor (20); and a distance information analysis module (40) providing correction data to improve accuracy of the posture angle by analyzing the posture angle of the wind tunnel test model (100). The posture angle of the wind tunnel test model (100), which should be measured by the contactless distance measurement sensor (20) based on a rotation center axis, is accurately set. Aerodynamic data of a wing deformed due to aerodynamics can be accurately obtained since a wind tunnel test is performed in a similar test condition as an actual flight condition by setting the accurate posture angle. |
申请公布号 |
KR101589568(B1) |
申请公布日期 |
2016.01.28 |
申请号 |
KR20140112394 |
申请日期 |
2014.08.27 |
申请人 |
AGENCY FOR DEFENSE DEVELOPMENT |
发明人 |
LEE, YEONG BIN;OH, SE YOON;LEE, JONG GEON;KIM, YOUNG JOON |
分类号 |
G01M9/04;G01M9/06 |
主分类号 |
G01M9/04 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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