顾蕴松
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Gender:Male
Education Level:南京航空航天大学
Alma Mater:南京航空航天大学
Scientific Research
Current position:
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Scientific Research
Research Field
Paper Publications
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Jianglong Guo, Yunsong Gu*, Linkai Li, Shilong Wang, Yuzhe Zhang. Normal force and pitching moment trend sensing of delta wing based on flow physical topology with sparse pressure measurements[J], Journal of Aerospace Engineering, 2025.01
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Zhou Y ,Gu Y ,Xue L , et al.Research on the control of supersonic jet under different boundary conditions[J].Journal of Visualization,2024,27(1):19-32.
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Zhou Y ,Gu Y ,Li L , et al.Research on fluidic thrust vector technology based on passive secondary flow with dual inclined walls under low subsonic speed[J].Experimental Thermal and Fluid Science,2024,155111200-.
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Xu D, Gu Y, Li W, et al. Experimental Investigation of the Performance of a Novel Ejector–Diffuser System with Different Supersonic Nozzle Arrays[J]. Fluids, 2024, 9(7): 155.
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Shi, N.; Gu, Y.; Wu, T.; Zhou, Y.; Wang, Y.; Deng, S. An Optimized Pressure-Based Method for Thrust Vectoring Angle Estimation[J]. Aerospace 2023, 10, 978.https://doi.org/10.3390/aerospace10120978
Patents
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顾蕴松,李琳恺,白亚磊,等.一种基于振荡射流激励器的飞行器垂直尾翼装置及飞行器[P].江苏省:CN202420522204.0,2024-10-29.
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李琳恺,顾蕴松,王傲,等.一种飞行器舵面状态实时感知方法及感知系统[P].江苏省:CN202311691686.9,2024-04-12.
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顾蕴松,郭江龙,李琳恺,等.一种用于飞行器的法向力/俯仰力矩实时感知系统及方法[P].江苏省:CN202311387881.2,2024-02-09.
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顾蕴松,史楠星,李琳恺,等.基于喷流状态感知的流体推力矢量喷管系统和控制方法[P].江苏省:CN202310691940.9,2023-11-21.
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顾蕴松,周宇航,史楠星,等.一种喉道背压调控下的喷管出口马赫数的控制装置[P].江苏省:CN202310275717.6,2023-06-13.