Boundary-layer transition of advanced fighter wings at high-speed cruise conditions
accepted 5 April 2018Available online 11 February 2019* Corresponding author.Peer review under responsibility of Editorial Committee of CJA.
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The present research was supported by the National Natural Science Foundation of China No. 11372254. The authors wish to thank Dr. Chuang WEI and Meng WANG of AVI-CARI, Shenyang, China, for their industrious work and pro-fessional analysis about the results of the wind-tunnel test;Dr. Shengyang NIE of Xi’an University of Technology for his warm concern and valuable discussion around the transi-tion mechanism and modeling. Heartfelt respect and thanks are expressed to anonymous reviewers for their precise and constructive comments on the present work
2019-09-27（万方平台首次上网日期，不代表论文的发表时间）
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799-814
