摘要
主要介绍了JL-6飞机抖振边界试飞的试验技术、测试技术和数据处理技术,给出了JL-6飞机的抖振边界试飞结果;介绍了JL-6飞机的抖振风洞试验的试验技术、试验条件和抖振边界风洞试验结果;利用风洞试验和飞行试验得到的数据进行了JL-6飞机抖振边界相关性分析。
This paper presented the experimental technique, measurement technique and data processing method of the flight buffet boundary test taking the use of JL-6 aircraft flight tests. And this paper showed the flight buffet boundary test results for the JL-6 aircraft. In addition, wind tunnel buffet test technique, test conditions and test results for the JL-6 aircraft were investigated. Furthermore, the buffet boundary correlation for the JL-6 aircraft was analyzed using the data obtained from wind tunnel tests and the flight test data of the JL-6 aircraft.
出处
《飞行力学》
CSCD
北大核心
2010年第2期85-88,共4页
Flight Dynamics
关键词
抖振
抖振边界
风洞试验
飞行试验
相关性
buffet
buffet boundary
wind tunnel test
flight test
correlation
