Yifan Zhao
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Research Subjects
Yifan Zhao has a total of 5 co-authors. Here are the top co-authors by number of shared publications:
- Jiaxi Zhao
Aerodynamic Noise Control Research Center, State Key Laboratory of Aerodynamic, China, Mianyang 621000, China
1 shared publication - Pengfei Yan
Aerodynamic Noise Control Research Center, State Key Laboratory of Aerodynamic, China, Mianyang 621000, China
1 shared publication - Rongping Zhang
Aerodynamic Noise Control Research Center, State Key Laboratory of Aerodynamic, China, Mianyang 621000, China
1 shared publication - Xunnian Wang
Aerodynamic Noise Control Research Center, State Key Laboratory of Aerodynamic, China, Mianyang 621000, China
1 shared publication - Yuxiang Liang
Aerodynamic Noise Control Research Center, State Key Laboratory of Aerodynamic, China, Mianyang 621000, China
1 shared publication
Latest Publications
- Open Access
Analysis of Flow Field Structure Characteristics of Dual Impinging Jets at Different Velocities
The flow structure and unsteady evolution characteristics of dual impinging jets represent a flow problem of significant engineering importance in the aerospace field. Currently, there is a lack of systematic research on the unsteady characteristics and the underlying mechanisms of flow structure evolution in dual impinging jets across different velocity regimes. This study investigates a dual impinging jet configuration with a nozzle pressure ratio ranging from 1.52 to 2.77, an impingement spacing of 5d (where d is the nozzle exit diameter), and an inter-nozzle spacing of 10.42d. By employing Particle Image Velocimetry and Proper Orthogonal Decomposition, the evolution of the flow field structure from subsonic to supersonic conditions is systematically analyzed. The results demonstrate that the fountain motion is composed of an anti-symmetric oscillatory mode, a symmetric breathing mode, and an intermittent transport mode. The upper confinement plate obstructs the fountain motion to some extent, inducing unsteady oscillation modes. An increase in jet velocity enhances the upwash momentum of the fountain and raises the characteristic frequencies of its dynamic structures. This research elucidates the influence of jet velocity variation on the flow field structure, providing a theoretical basis for formulating flow control strategies in related engineering applications.
Open AccessAnalysis of Flow Field Structure Characteristics of Dual Impinging Jets at Different Velocities
The flow structure and unsteady evolution characteristics of dual impinging jets represent a flow problem of significant engineering importance in the aerospace field. Currently, there is a lack of systematic research on the unsteady characteristics and the underlying mechanisms of flow structure evolution in dual impinging jets across different velocity regimes. This study investigates a dual impinging jet configuration with a nozzle pressure ratio ranging from 1.52 to 2.77, an impingement spacing of 5d (where d is the nozzle exit diameter), and an inter-nozzle spacing of 10.42d. By employing Particle Image Velocimetry and Proper Orthogonal Decomposition, the evolution of the flow field structure from subsonic to supersonic conditions is systematically analyzed. The results demonstrate that the fountain motion is composed of an anti-symmetric oscillatory mode, a symmetric breathing mode, and an intermittent transport mode. The upper confinement plate obstructs the fountain motion to some extent, inducing unsteady oscillation modes. An increase in jet velocity enhances the upwash momentum of the fountain and raises the characteristic frequencies of its dynamic structures. This research elucidates the influence of jet velocity variation on the flow field structure, providing a theoretical basis for formulating flow control strategies in related engineering applications.