In order to choosing right model support, support interference of rear sting and Zsting was experimentally investigated in a highspeed wind tunnel. The experimental results show that the sting support interference is not small enough to be neglected. The interference on lift,drag and pitching moment coefficient changes lineally with the model attack angle. The rear sting is so close to model that it affects the flow field on model empennage. The Zsting brings little effect on model empennage, so the interference of whole model is similar with that of the model without empennage.
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巴玉龙,白峰.高速风洞模型支撑方式研究[J].民用飞机设计与研 究,2016(4):50-BA Yulong, BAI Feng. Research of Sting Support in Highspeed WindTunnel Test[J]. Civil Aircraft Design and Research,2016,(4):50-. ( in Chinese)