Investigation on wing rock in low speed wind tunnel for a fighter configuration

SUN Hai-sheng; JIANG Yu-biao

doi:10.3969/j.issn.1672-9897.2000.04.006

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Article Navigation > Journal of Experiments in Fluid Mechanics > 2000 > 14(4): 32-35

SUN Hai-sheng, JIANG Yu-biao. Investigation on wing rock in low speed wind tunnel for a fighter configuration[J]. Journal of Experiments in Fluid Mechanics, 2000, 14(4): 32-35. doi: 10.3969/j.issn.1672-9897.2000.04.006

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Investigation on wing rock in low speed wind tunnel for a fighter configuration

doi: 10.3969/j.issn.1672-9897.2000.04.006

Publish Date: 2000-04-01

Abstract

Abstract

The wing rock test technique in low speed wind tunnel is presented in this paper, including test apparatus and test methods as well as data acquisition. The typical test results about wing rock for a fighter configuration conducted in CARDC 4m × 3m low speed wind tunnel are also discussed briefly. Finally, the mechanism of wing rock is explored.

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