In order to study the interaction between two independent jets, a three-dimensional（3D） transient mathematical model is developed to investigate the flow field and acoustic properties of the two-stream jets. The res...In order to study the interaction between two independent jets, a three-dimensional（3D） transient mathematical model is developed to investigate the flow field and acoustic properties of the two-stream jets. The results are compared with those of the single-stream jet at Mach number 0.9 and Reynolds number 3600. The large eddy simulation（LES） with dynamic Smagorinsky sub-grid scale（SGS） approach is used to simulate the turbulent jet flow structure. The acoustic field is evaluated by the Ffowcs Williams–Hawkings（FW-H） integral equation. Considering the compressibility of high-speed gas jets, the density-based explicit formulation is adopted to solve the governing equations. Meanwhile, the viscosity is approximated by using the Sutherland kinetic theory. The predicted flow characteristics as well as the acoustic properties show that they are in good agreement with the existing experimental and numerical results under the same flow conditions available in the literature. The results indicate that the merging phenomenon of the dual-jet is triggered by the deflection mechanism of the Coanda effect, which sequentially introduces additional complexity and instability of flow structure. One of the main factors affecting the dual-jet merging is the aperture ratio, which has a direct influence on the potential core and surrounding flow fluctuation. The analysis on the noise pollution reveals that the potential core plays a fundamental role in noise emission while the additional mixing noise makes less contribution than the single jet noise. The overall sound pressure level（OASPL） profiles have a directive property, suggesting an approximate 25° deflection from the streamwise direction, however, shifting toward lateral direction of about 10° to 15° in the dual-jet. The conclusion obtained in this study can provide valuable data to guide the development of manufacturing-green technology in the multi-jet applications.展开更多
A dual-jet consisting of a wall jet and an offset jet has been numerically simulated using lattice Boltzmann method to examine the effects of jet spacing between two jet centerlines,defined as s.The Reynolds number ba...A dual-jet consisting of a wall jet and an offset jet has been numerically simulated using lattice Boltzmann method to examine the effects of jet spacing between two jet centerlines,defined as s.The Reynolds number based on jet-exit-width dis set to be Re = 56 and the jet spacing is set to be less than or equal 10 times the jet-exitwidth.Computational results reveal that the flow field displays periodic vortex shedding when the jet spacing is in the range of 9≤s/d ≤ 10,while it remains steady with two counter-rotating vortices in the converging region when s/d ≤ 8.When s/d = 9,the power spectral analyses indicate that the vortex shedding phenomenon has specific frequency.The significant oscillation stresses induced by the periodic components of velocities are found to mainly exist in the inner shear layer regions,implying stronger momentum transfer occuring in these regions.展开更多
This work reports the analysis of the flow characteristics of two plane,parallel jets that merge as they issue into stagnant surroundings.The predicted results based on a simple integral analysis of the flowfield are ...This work reports the analysis of the flow characteristics of two plane,parallel jets that merge as they issue into stagnant surroundings.The predicted results based on a simple integral analysis of the flowfield are compared with the experimental data.It shows that the simple analysis predicts the major variables of the dual-jet reasonably well and the spreading parameter σ=15 for plane dual-jet.展开更多
锯齿形喷嘴被认为是一种有效而实用的射流噪声被动控制方法。采用大涡模拟与FW-H方程(Ffowcs Williams and Hawkings Equation)相结合的方法预测圆形喷口和锯齿型喷口的流场和远场噪声。分析锯齿的分布方式以及结构参数对降噪特性的影...锯齿形喷嘴被认为是一种有效而实用的射流噪声被动控制方法。采用大涡模拟与FW-H方程(Ffowcs Williams and Hawkings Equation)相结合的方法预测圆形喷口和锯齿型喷口的流场和远场噪声。分析锯齿的分布方式以及结构参数对降噪特性的影响。结果表明,尾喷管的射流核心区域温度较高,湍动能值较小,整个核心区域呈现锥形。锯齿型喷口可以有效抑制低频段喷流噪声;仅在内涵添加锯齿结构的喷口降噪效果最好,可以降低整个频段的噪声;齿数增加与切入角变化对降噪效果有一定影响。展开更多
基金Project supported by the Fundamental Research Funds for the Central Universities,China(Grant No.N150204003)
文摘In order to study the interaction between two independent jets, a three-dimensional（3D） transient mathematical model is developed to investigate the flow field and acoustic properties of the two-stream jets. The results are compared with those of the single-stream jet at Mach number 0.9 and Reynolds number 3600. The large eddy simulation（LES） with dynamic Smagorinsky sub-grid scale（SGS） approach is used to simulate the turbulent jet flow structure. The acoustic field is evaluated by the Ffowcs Williams–Hawkings（FW-H） integral equation. Considering the compressibility of high-speed gas jets, the density-based explicit formulation is adopted to solve the governing equations. Meanwhile, the viscosity is approximated by using the Sutherland kinetic theory. The predicted flow characteristics as well as the acoustic properties show that they are in good agreement with the existing experimental and numerical results under the same flow conditions available in the literature. The results indicate that the merging phenomenon of the dual-jet is triggered by the deflection mechanism of the Coanda effect, which sequentially introduces additional complexity and instability of flow structure. One of the main factors affecting the dual-jet merging is the aperture ratio, which has a direct influence on the potential core and surrounding flow fluctuation. The analysis on the noise pollution reveals that the potential core plays a fundamental role in noise emission while the additional mixing noise makes less contribution than the single jet noise. The overall sound pressure level（OASPL） profiles have a directive property, suggesting an approximate 25° deflection from the streamwise direction, however, shifting toward lateral direction of about 10° to 15° in the dual-jet. The conclusion obtained in this study can provide valuable data to guide the development of manufacturing-green technology in the multi-jet applications.
基金supported by the National Natural Science Foundation of China(No.11402124)the Natural Science Foundation of Jiangsu Province(No.BK20140985)+1 种基金the Natural Science Foundation of Jiangsu Higher Education Institutions of China(No.14KJB130002)the Startup Foundation for Introducing Talent of NUIST(No.2013x031)
文摘A dual-jet consisting of a wall jet and an offset jet has been numerically simulated using lattice Boltzmann method to examine the effects of jet spacing between two jet centerlines,defined as s.The Reynolds number based on jet-exit-width dis set to be Re = 56 and the jet spacing is set to be less than or equal 10 times the jet-exitwidth.Computational results reveal that the flow field displays periodic vortex shedding when the jet spacing is in the range of 9≤s/d ≤ 10,while it remains steady with two counter-rotating vortices in the converging region when s/d ≤ 8.When s/d = 9,the power spectral analyses indicate that the vortex shedding phenomenon has specific frequency.The significant oscillation stresses induced by the periodic components of velocities are found to mainly exist in the inner shear layer regions,implying stronger momentum transfer occuring in these regions.
文摘This work reports the analysis of the flow characteristics of two plane,parallel jets that merge as they issue into stagnant surroundings.The predicted results based on a simple integral analysis of the flowfield are compared with the experimental data.It shows that the simple analysis predicts the major variables of the dual-jet reasonably well and the spreading parameter σ=15 for plane dual-jet.
文摘锯齿形喷嘴被认为是一种有效而实用的射流噪声被动控制方法。采用大涡模拟与FW-H方程(Ffowcs Williams and Hawkings Equation)相结合的方法预测圆形喷口和锯齿型喷口的流场和远场噪声。分析锯齿的分布方式以及结构参数对降噪特性的影响。结果表明,尾喷管的射流核心区域温度较高,湍动能值较小,整个核心区域呈现锥形。锯齿型喷口可以有效抑制低频段喷流噪声;仅在内涵添加锯齿结构的喷口降噪效果最好,可以降低整个频段的噪声;齿数增加与切入角变化对降噪效果有一定影响。
