Characterization of the aircraft bay/landing gear coupling noise at low subsonic speeds and its suppression using leading-edge chevron spoiler von Zhao, Kun, Liang, Yong, Yue, Tingrui, Chen, Zhengwu, Bennett, Gareth J

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Deformation Measurements of Helicopter Rotor Blades Using a Photogrammetric System von Zuo, Chenglin, Ma, Jun, Wei, Chunhua, Yue, Tingrui, Song, Jin

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Full-Field Displacement Measurements of Helicopter Rotor Blades Using Stereophotogrammetry von Zuo, Chenglin, Wei, Chunhua, Ma, Jun, Yue, Tingrui, Liu, Lei, Shi, Zheyu

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Application of stereo PIV to the 70° delta wing at subsonic speed von Wei, Chunhua, Zuo, Chenglin, Liang, Lei, Yue, Tingrui, Cheng, Yong

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Standing wave and its impact on the low-frequency pressure fluctuation in an open jet wind tunnel von Jin, Ling, Gu, Yunsong, Deng, Xiao Bing, Sun, Haisheng, Yue, Tingrui, Zhang, Junlong

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Method for realizing conversion from balance certificate to program general code in wind tunnel test von LIU ZHONGHUA, YUE TINGRUI

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Dielectric barrier discharge plasma induced airflow temperature field measuring device and method von LI CHANG, ZHANG XIN, YUE TINGRUI

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Method for detecting pressure uniformity of laminating machine von CHENG HAO, HE JIANGQI, YUAN QIANG, YUE TINGRUI

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Braided circuit board and manufacturing method thereof von ZHANG GAO, HE JIANGQI, YUAN QIANG, YUE TINGRUI

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Device and experimental method for detecting dynamic transition position of airfoil profile von LI GUOQIANG, LI TINGTING, CHE BINGHUI, SONG KUIHUI, WU LINXIN, YUE TINGRUI

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Laser ray extraction fusion and online ice shape measurement method for measuring ice shape von ZUO CHENGLIN, LIU SENYUN, MA JUN, WEI LONGTAO, ZHAO RONG, YUE TINGRUI

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Icing thickness measuring method and system based on far-field sound pressure level change von XIAO CHUNHUA, CHE BINGHUI, ZHANG XUN, MA SHUAI, YUE TINGRUI

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Blade model surface pressure sensor internal wire fixing device and method von WANG CHANG, YIN XIWEI, LIANG YONG, ZHANG WEIGUO, YUAN HONGGANG, YANG NINGMENG, ZHANG JUN, MA SHUAI, YUE TINGRUI

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Aircraft model surface mark point matching method von JIANG YUBIAO, YIN XIWEI, WEI CHUNHUA, ZUO CHENGLIN, LIANG LEI, MA JUN, YUE TINGRUI

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Aircraft model surface mark point positioning method von JIANG YUBIAO, YIN XIWEI, WEI CHUNHUA, ZUO CHENGLIN, LIANG LEI, MA JUN, YUE TINGRUI

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Low-speed wind tunnel rotor model variable azimuth angle surface pressure measurement system and method von YIN XIWEI, WEI CHUNHUA, ZHANG WEIGUO, ZUO CHENGLIN, LIANG LEI, YUE TINGRUI

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Helicopter rotor blade deformation and surface pressure synchronous measurement device and method von LIU LEI, YIN XIWEI, WEI CHUNHUA, ZUO CHENGLIN, LIANG LEI, YUE TINGRUI

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All-optical BEC preparation method based on three-dimensional Raman sideband cooling von LIU LEI, YIN XIWEI, WEI CHUNHUA, ZUO CHENGLIN, LIANG LEI, MA JUN, YUE TINGRUI

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Wind tunnel fixed wing model surface pulsating pressure measuring method von LIU LEI, YIN XIWEI, WEI CHUNHUA, ZUO CHENGLIN, LIANG LEI, MA JUN, YUE TINGRUI

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Helicopter blade mark point identification matching method based on position constraint von LIU LEI, WANG XUNNIAN, ZHANG WEIGUO, ZUO CHENGLIN, MA JUN, SHI ZHEYU, YUE TINGRUI

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