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L8飞机从风洞到飞行的抖振相关性研究
引用本文:张雪佩. L8飞机从风洞到飞行的抖振相关性研究[J]. 洪都科技, 1995, 0(4): 1-8
作者姓名:张雪佩
作者单位:650所
摘    要:介绍了L8飞机抖振边界修正结果,并与同类飞机L29飞行抖振边界进行了比较;给出了L8飞机抖振边和轻度抖振边界预测值。同时将预测抖振边界和试飞得到的抖振边界作了比较。

关 键 词:飞机 风洞试验 抖振边界

COHERENCE STUDY ON BUFFET OF L8 AIRCRAFT FROM WIND-TUNNEL TEST TO FLIGHT TEST
Zhang Xuepi. COHERENCE STUDY ON BUFFET OF L8 AIRCRAFT FROM WIND-TUNNEL TEST TO FLIGHT TEST[J]. Hongdu Science and Technology, 1995, 0(4): 1-8
Authors:Zhang Xuepi
Affiliation:NO.650 Institute
Abstract:This paper describes the correction result of L8 A/C buffet along with the comparison with that of L29 A/C in the same family,and presents the cstimated value of L8 A/C buffet boundary and gentle buffet boundary . Moreover it compares the estimated buffet boundary with that gained from the flight test.
Keywords:L8 Aircraft  Wind Tunnel Test  Buffet Boundary
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