Sharp Cone Boundary Layer Transition in Arc Heated Flow Field

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Sharp Cone Boundary Layer Transition in Arc Heated Flow Field
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Key words:尖锥%边界层转捩%电弧加热%雷诺数

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[3]王义乾,LIU Chaoqun,赵宁.Motion Around Vortices and Λ Vortex Rings in Boundary Layer Transition[J].Aeronautical Computer Technique,2016(2):15-18.

[4]Fan,Jiechuan.Flow Visualization and Measurement Technique of Boundary Layer Transition Used in Flight Test[J].Flight Dynamics,1998,16(1):80-84.

[5]FENG Guo-tai,ZHANG Yong-jun,CHEN Fu and SU Jie-xian.Influence of Inlet Boundary Layer on Flow Field Performance of the 2D Compressor Bowed Stator Vane[J].Journal of Aerospace Power,2006,21(2):254-260.

[6]LIANG Yun,LIU Huo-xing and ZOU Zheng-ping.Experimental Investigation on Boundary Layer Transition Process in High-Lift Low-Pressure Turbines[J].Journal of Propulsion Technology,2017,38(5):1023-1029.

[7]Numerical Simulation of Wake-Induced Boundary Layer Transition in Low-Pressure Turbine[J].Gas Turbine Experiment and Research

[8]LI Hong-yang and ZHENG Yun.Effects of Wake on Boundary Layer Transition of Turbine Cascade[J].Journal of Propulsion Technology,2017,38(3):532-538.

[9]Zhang Qingli,Li Jingbai.Control of Boundary Layer Transition Using Active Compliant Wall Motion[J].Acta Aerodynamica Sinica,1999,17(3):333-338.

[10]ZHANG Hong-jun,YUAN Xiang-jiang and SHEN Qing.Analysis on Boundary Layer Flow Stability of Hypersonic Wedge[J].Journal of Propulsion Technology,2012,33(5):671-675.

[11]Flow Field of Double Layer Atomizer[J].Journal of Aeronautical Materials

[12]wusi and Gao Zhenghong.Analysis of Airfoil Geometry Model on Boundary Layer Transition Prediction[J].Advances in Aeronautical Science and Engineering,2015,6(3):287-296.

[13]Li Jingbai.Boundary Layer Transition Controlled by Acoustic Excitation Disturbances[J].Acta Aerodynamica Sinica,1994,12(2):165-170.

[14]Zeng Honggang,Chen Jiaojiao,Zhou Ling,Qu Feng,Yi Shihe,Zhang Feng.Application of Transition Mode and Experiment on Hypersonic Boundary Layer Transition[J].Aeronautical Science and Technology,2020,31(11):113-119.

[15]Yuan Xiangjiang,Zhou Heng,Hao Gengfu.Stability Characteristics of the Boundary Layer of an Axisymmetric Blunt Nosed Cone in the Supersonic and Hypersonic Flow[J].Acta Aerodynamica Sinica,1999,17(1):98-104.

[16]WANG Weixing,GUO Rongwei.Study of Flow Characteristics of Hypersonic Inlet Based on Boundary Layer Transition[J].Acta Aeronautica et Astronautica Sinica,2012,33(10):1772-1780.

[17]Li Jingbai.An Investigation of Boundary Layer Transition Controlled by Internal Acoustic Excitation[J].Acta Aerodynamica Sinica,1992,10(3):305-311.

[18]PAN Hong-lu,MA Han-dong,WANG Qiang.Large Eddy Simulation of Transition in a Hypersonic Blunt-wedge Boundary Layer[J].Acta Aeronautica et Astronautica Sinica,2007,28(2):269-274.

[19]DU Kun and WANG Song-tao.Effects of Rotor-Stator Interaction on Flow Field of a Transonic Boundary Layer Suction Compressor[J].Journal of Propulsion Technology,2015,36(5):713-721.

[20]ZHAO Jian,FAN Xiao-qiang,WANG Yi,TAO Yuan and LI Teng-ji.Classification of Flow Field in Supersonic Boundary Layer Bleed Slot[J].Journal of Propulsion Technology,2017,38(11):2463-2470.

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