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Design of supercritical natural laminar flow wing and its boundary layer transition wind tunnel test based on TSP technique
ZHANG Yanjun, DUAN Zhuoyi, LEI Wutao, BAI Junqiang, XU Jiakuan
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2019, (
4
): 122429 -122429 . DOI: 10.7527/S1000-6893.2018.22429