为了研究柱体结构的涡激振动特性预测方法,首先基于Van der Pol尾流振子模型建立了弹性支撑单自由度柱体的涡激振动模型。然后基于计算流体力学(CFD)方法、结构动力学理论以及嵌套网格技术,同时考虑弹性支撑柱体来流向和横向振动,建立...为了研究柱体结构的涡激振动特性预测方法,首先基于Van der Pol尾流振子模型建立了弹性支撑单自由度柱体的涡激振动模型。然后基于计算流体力学(CFD)方法、结构动力学理论以及嵌套网格技术,同时考虑弹性支撑柱体来流向和横向振动,建立了柱体结构的涡激振动高保真仿真模型。通过与国外文献实验数据对比,验证了两种模型的准确性。计算结果表明,在低质量比情况下,Van der Pol尾流振子模型在约化速度较小区域计算误差很大,在柱体振幅最大值附近误差较小,基本上可以捕捉到柱体的涡激振动特性,可以用于工程上快速预测柱体结构的涡激振动特性;在低质量比、高质量比以及指定的约化速度范围内,采用CFD方法和嵌套网格技术,可以避免由于柱体振幅较大引起的网格畸变和负网格问题,且可以获得较好的计算精度和详细的流场信息,但计算效率相比Van der Pol尾流振子模型较低。展开更多
LoRaWAN是一种具有代表性的低功耗广域网(LPWAN,low power wide area network)技术,受到了业界和学术界的高度关注。在物联网(IoT,Internet of things)新时代,LoRaWAN可以极大地提高海量边缘设备的连接能力。简要回顾了LoRaWAN的基础知...LoRaWAN是一种具有代表性的低功耗广域网(LPWAN,low power wide area network)技术,受到了业界和学术界的高度关注。在物联网(IoT,Internet of things)新时代,LoRaWAN可以极大地提高海量边缘设备的连接能力。简要回顾了LoRaWAN的基础知识,并从通信性能、目标定位、无线网络安全和混合网络4个方面调研了LoRaWAN的最新研究成果。还从商业模式、监管制度、技术创新和新兴应用4个方面讨论了LoRaWAN在中国发展所面临的机遇和挑战。展开更多
Aerodynamic noise is the main problem restricting its development nowadays in green energy,ocean engineering and aerospace engineering.In order to limit the aerodynamic noise of an airfoil structure,a method is propos...Aerodynamic noise is the main problem restricting its development nowadays in green energy,ocean engineering and aerospace engineering.In order to limit the aerodynamic noise of an airfoil structure,a method is proposed in this paper by designing low noise airfoils.This method optimized the aerodynamic noise of two-dimensional airfoil,and considered the aerodynamic performance of the airfoil at the same time.Based on Joukowski conformal transformation,airfoil geometry is parameterized firstly.Then,the optimization model taking the lift-to-drag ratio and airfoil self-noise as the design objective,is established to modify the airfoil by active set algorithm until the airfoil can satisfy the design condition.Finally,the noise of the optimized airfoil is verified according to the prediction theory of airfoil noise.Moreover,the relationship between airfoil geometry and noise is analyzed.The results show that the lift-to-drag ratio of the optimized airfoil increased,and the noise also decreased.Thus,the optimization method can be used to address special design of low-noise airfoil.Besides,the optimization method in this paper can provide reference for improving lift-to-drag ratio and reducing noise of the airfoil in aircraft and submarine rudder system.展开更多
文摘为了研究柱体结构的涡激振动特性预测方法,首先基于Van der Pol尾流振子模型建立了弹性支撑单自由度柱体的涡激振动模型。然后基于计算流体力学(CFD)方法、结构动力学理论以及嵌套网格技术,同时考虑弹性支撑柱体来流向和横向振动,建立了柱体结构的涡激振动高保真仿真模型。通过与国外文献实验数据对比,验证了两种模型的准确性。计算结果表明,在低质量比情况下,Van der Pol尾流振子模型在约化速度较小区域计算误差很大,在柱体振幅最大值附近误差较小,基本上可以捕捉到柱体的涡激振动特性,可以用于工程上快速预测柱体结构的涡激振动特性;在低质量比、高质量比以及指定的约化速度范围内,采用CFD方法和嵌套网格技术,可以避免由于柱体振幅较大引起的网格畸变和负网格问题,且可以获得较好的计算精度和详细的流场信息,但计算效率相比Van der Pol尾流振子模型较低。
文摘LoRaWAN是一种具有代表性的低功耗广域网(LPWAN,low power wide area network)技术,受到了业界和学术界的高度关注。在物联网(IoT,Internet of things)新时代,LoRaWAN可以极大地提高海量边缘设备的连接能力。简要回顾了LoRaWAN的基础知识,并从通信性能、目标定位、无线网络安全和混合网络4个方面调研了LoRaWAN的最新研究成果。还从商业模式、监管制度、技术创新和新兴应用4个方面讨论了LoRaWAN在中国发展所面临的机遇和挑战。
基金Supported by the Natural Science Foundation of Jiangsu Province(BK20190871)the National Natural Science Foundation of China(11672261)。
文摘Aerodynamic noise is the main problem restricting its development nowadays in green energy,ocean engineering and aerospace engineering.In order to limit the aerodynamic noise of an airfoil structure,a method is proposed in this paper by designing low noise airfoils.This method optimized the aerodynamic noise of two-dimensional airfoil,and considered the aerodynamic performance of the airfoil at the same time.Based on Joukowski conformal transformation,airfoil geometry is parameterized firstly.Then,the optimization model taking the lift-to-drag ratio and airfoil self-noise as the design objective,is established to modify the airfoil by active set algorithm until the airfoil can satisfy the design condition.Finally,the noise of the optimized airfoil is verified according to the prediction theory of airfoil noise.Moreover,the relationship between airfoil geometry and noise is analyzed.The results show that the lift-to-drag ratio of the optimized airfoil increased,and the noise also decreased.Thus,the optimization method can be used to address special design of low-noise airfoil.Besides,the optimization method in this paper can provide reference for improving lift-to-drag ratio and reducing noise of the airfoil in aircraft and submarine rudder system.
