栾爽
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Education Level:南京师范大学
Scientific Research
Current position:
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Scientific Research
Research Field
主要从事发动机内流气动力学、宽速域高超声速飞行器推进系统、复杂流场的先进测量技术、流动控制与气动矢量喷管等研究工作。
Paper Publications
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Xu Jinglei. 平行四边形截面的旁路式双喉道气动矢量喷管数值研究.航空动力学报.2020
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qiweicheng. Numerical simulation and experimental calibration of continuously adjustable wind tunnel with Mach number 2 to 4.Hangkong Xuebao.2017
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俞凯凯. New adaptive sampling method in particle image velocimetry.Measurement Science and Technology.2015,26(3):1385-1389
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Xu Jinglei. Research Progress of Nozzle Design Method for Scramjet and Turbine Based Combined Cycle.Tuijin Jishu.2018
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Xu Jinglei. Experiment on effects of slotted tailboard on flow field of transonic turbine linear cascade.Hangkong Dongli Xuebao.2018
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Xu Jinglei. Computational study of axisymmetric divergent bypass dual throat nozzle.Aerosp Sci Technol.2019