高超声速风洞气动力试验技术进展
收稿日期: 2014-07-25
修回日期: 2014-10-31
网络出版日期: 2014-10-31
Research progress on hypersonic wind tunnel aerodynamic testing techniques
Received date: 2014-07-25
Revised date: 2014-10-31
Online published: 2014-10-31
唐志共 , 许晓斌 , 杨彦广 , 李绪国 , 戴金雯 , 吕治国 , 贺伟 . 高超声速风洞气动力试验技术进展[J]. 航空学报, 2015 , 36(1) : 86 -97 . DOI: 10.7527/S1000-6893.2014.0229
The hypersonic technology is the summit of aeronautics and astronautics techniques in the near future, and the hypersonic wind tunnel aerodynamic force test would be an indispensable measure to provide valuable data for the estimation and evaluation of hypersonic vehicle designing and aerodynamic characters. The hypersonic aerodynamic test facilities and development status of China are introduced in this paper, as well as measurement techniques, test methods, test data analysis technique and hypersonic aerodynamic calibration model system development. Besides, the development trends of hypersonic aerodynamic test facilities and aerodynamic testing involved techniques are discussed in the paper.
Key words： hypersonic; wind tunnel; aerodynamic force; testing technique; measurement technique
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