为探索增强小迎角下翼型气动性能的射流控制方法,进而实现无舵飞行控制,在环量控制的启发下,提出在NACA0012翼型下表面靠近后缘的位置布置射流(Jet on the lower surface of trailing edge,LSTE jet),并通过分析流动状态与参数变化优化L...为探索增强小迎角下翼型气动性能的射流控制方法,进而实现无舵飞行控制,在环量控制的启发下,提出在NACA0012翼型下表面靠近后缘的位置布置射流(Jet on the lower surface of trailing edge,LSTE jet),并通过分析流动状态与参数变化优化LSTE射流的气动控制效果.首先,采用3套不同规模的网格对NACA0012翼型本身进行数值模拟,验证了数值模拟方法的收敛性与有效性.其次,通过比较流场的马赫数分布、流线和压力分布的变化,研究了LSTE射流影响翼型气动性能的机理.最后,研究了翼型的气动系数随射流的位置、动量系数和前向夹角的变化规律.结果表明:LSTE射流在后缘诱导产生逆时针的涡,形成低压分离区,使后缘主流向下偏折,增加了翼型的有效弯度,并且前缘的吸力峰也因此增加,从而增大了升力系数;LSTE射流越靠近后缘,动量系数越大,增升减阻效果越好,但翼型的失速迎角会减小1°~3°;在不同的迎角和射流动量系数下,翼型的最大升力和最小阻力可以同时在γ=60°~70°之间达到.利用LSTE射流可以有效改变小迎角下翼型的气动性能,对实现飞行器无舵操纵有一定意义.展开更多
Shock wave/boundary layer interaction in a 24°turning angle of the compression ramp at Mach number 2.9 controlled by steady microjet is investigated using direct numerical simulation.Three different jet spacings ...Shock wave/boundary layer interaction in a 24°turning angle of the compression ramp at Mach number 2.9 controlled by steady microjet is investigated using direct numerical simulation.Three different jet spacings which are termed as sparse,moderate and dense are considered,and the induced vortex system and shock structures are compared.A moderate jet spacing configuration is found to generate counter-rotating vortex pairs that transport high-momentum fluid towards the vicinity of wall and strengthen the boundary layer to resist separation,reducing the separation region.The dense jet spacing configuration creates a larger momentum deficit region,reducing the friction downstream of the corner.Analysis of pressure and pressure gradient reveals that dense jet spacing configuration reduces the intensity of separation shock.The impact of varying jet spacings on the turbulent kinetic energy transport mechanism is also investigated by decomposing the budget terms in the transport equation.Furthermore,the spectral characteristics of the separation region are studied using power spectral density and dynamic mode decomposition methods,revealing that moderate jet spacing configuration suppresses low-frequency fluctuations in the separation region.展开更多
The fractal dimensions of turbulent round jets in steady crossflow has been analyzed by using planar laser-induced fluorescence (PLIF) method. The relation between the fractal dimension and the momentum ratio, the var...The fractal dimensions of turbulent round jets in steady crossflow has been analyzed by using planar laser-induced fluorescence (PLIF) method. The relation between the fractal dimension and the momentum ratio, the variation of the fractal dimension with the elevation of jet and the dilution have been investigated. The comparison of the fractal characteristics between the multiple jets and the signal jet has been carried out.展开更多
On the hypothesis that the turbulent flow is practically not affected in character by pulsation of the flow, the formula for sound pressure level of pulsed jet noise is obtained in 90 °direction and 1 meter away ...On the hypothesis that the turbulent flow is practically not affected in character by pulsation of the flow, the formula for sound pressure level of pulsed jet noise is obtained in 90 °direction and 1 meter away from the nozzle. The steady jet noise is , then, a special case when the pulsating frequency is zero. The results agree well with experiments.展开更多
The possibility of using of pulsed supersonic gas jets for the formation of high intensity cluster ion beams are discusses. The results of experimental investigations of pulsed gases expansion are generalized in terms...The possibility of using of pulsed supersonic gas jets for the formation of high intensity cluster ion beams are discusses. The results of experimental investigations of pulsed gases expansion are generalized in terms of dimensionless similarity parameters. The results of the experimental study of formation of an high-intensity cluster beam of argon are presented. The fundamental phenomenon influences on the main parameters of cluster beam (cluster size, intensity ect.) are considered.展开更多
文摘为探索增强小迎角下翼型气动性能的射流控制方法,进而实现无舵飞行控制,在环量控制的启发下,提出在NACA0012翼型下表面靠近后缘的位置布置射流(Jet on the lower surface of trailing edge,LSTE jet),并通过分析流动状态与参数变化优化LSTE射流的气动控制效果.首先,采用3套不同规模的网格对NACA0012翼型本身进行数值模拟,验证了数值模拟方法的收敛性与有效性.其次,通过比较流场的马赫数分布、流线和压力分布的变化,研究了LSTE射流影响翼型气动性能的机理.最后,研究了翼型的气动系数随射流的位置、动量系数和前向夹角的变化规律.结果表明:LSTE射流在后缘诱导产生逆时针的涡,形成低压分离区,使后缘主流向下偏折,增加了翼型的有效弯度,并且前缘的吸力峰也因此增加,从而增大了升力系数;LSTE射流越靠近后缘,动量系数越大,增升减阻效果越好,但翼型的失速迎角会减小1°~3°;在不同的迎角和射流动量系数下,翼型的最大升力和最小阻力可以同时在γ=60°~70°之间达到.利用LSTE射流可以有效改变小迎角下翼型的气动性能,对实现飞行器无舵操纵有一定意义.
基金Supported by the National Natural Science Foundation of China(Nos.11972064,92052104)the Key Laboratory of Computational Aerodynamics,AVIC Aerodynamics Research Institute,China(No.YL2022XFX0405)the Fundamental Research Funds for the Central Universities,China.
文摘Shock wave/boundary layer interaction in a 24°turning angle of the compression ramp at Mach number 2.9 controlled by steady microjet is investigated using direct numerical simulation.Three different jet spacings which are termed as sparse,moderate and dense are considered,and the induced vortex system and shock structures are compared.A moderate jet spacing configuration is found to generate counter-rotating vortex pairs that transport high-momentum fluid towards the vicinity of wall and strengthen the boundary layer to resist separation,reducing the separation region.The dense jet spacing configuration creates a larger momentum deficit region,reducing the friction downstream of the corner.Analysis of pressure and pressure gradient reveals that dense jet spacing configuration reduces the intensity of separation shock.The impact of varying jet spacings on the turbulent kinetic energy transport mechanism is also investigated by decomposing the budget terms in the transport equation.Furthermore,the spectral characteristics of the separation region are studied using power spectral density and dynamic mode decomposition methods,revealing that moderate jet spacing configuration suppresses low-frequency fluctuations in the separation region.
文摘The fractal dimensions of turbulent round jets in steady crossflow has been analyzed by using planar laser-induced fluorescence (PLIF) method. The relation between the fractal dimension and the momentum ratio, the variation of the fractal dimension with the elevation of jet and the dilution have been investigated. The comparison of the fractal characteristics between the multiple jets and the signal jet has been carried out.
文摘On the hypothesis that the turbulent flow is practically not affected in character by pulsation of the flow, the formula for sound pressure level of pulsed jet noise is obtained in 90 °direction and 1 meter away from the nozzle. The steady jet noise is , then, a special case when the pulsating frequency is zero. The results agree well with experiments.
基金supported by the National Natural Science Foundation of China(Grant Nos.12202488 and 12002377)the Natural Science Program of National University of Defense Technology(Grant No.ZK22-30)Independent Cultivation Project for Young Talents in College of Aerospace Science and Engineering.
文摘The possibility of using of pulsed supersonic gas jets for the formation of high intensity cluster ion beams are discusses. The results of experimental investigations of pulsed gases expansion are generalized in terms of dimensionless similarity parameters. The results of the experimental study of formation of an high-intensity cluster beam of argon are presented. The fundamental phenomenon influences on the main parameters of cluster beam (cluster size, intensity ect.) are considered.