嵌入式大气数据传感系统(Flush Air Data Sensing System,FADS)通过在飞行器表面特定区域布置测压孔测量来流压力,根据建立的气动模型反推得到飞行参数(攻角、侧滑角、马赫数、静压及动压等)。利用在尖楔前体表面三维区中分布测压孔的方...嵌入式大气数据传感系统(Flush Air Data Sensing System,FADS)通过在飞行器表面特定区域布置测压孔测量来流压力,根据建立的气动模型反推得到飞行参数(攻角、侧滑角、马赫数、静压及动压等)。利用在尖楔前体表面三维区中分布测压孔的方法,根据三维区中的流动特征和压力分布规律,建立压力分布与飞行参数之间的关系。试验结果表明,基于三维区理论的FADS系统得到的马赫数误差在5%左右,精度较高。展开更多
The author reviews some recent developments in Chern-Simons theory on a hyperbolic 3-manifold M with complex gauge group G. The author focuses on the case of G = SL(N, C) and M being a knot complement: M = S^3\ K. The...The author reviews some recent developments in Chern-Simons theory on a hyperbolic 3-manifold M with complex gauge group G. The author focuses on the case of G = SL(N, C) and M being a knot complement: M = S^3\ K. The main result presented in this note is the cluster partition function, a computational tool that uses cluster algebra techniques to evaluate the Chern-Simons path integral for G = SL(N, C). He also reviews various applications and open questions regarding the cluster partition function and some of its relation with string theory.展开更多
文摘嵌入式大气数据传感系统(Flush Air Data Sensing System,FADS)通过在飞行器表面特定区域布置测压孔测量来流压力,根据建立的气动模型反推得到飞行参数(攻角、侧滑角、马赫数、静压及动压等)。利用在尖楔前体表面三维区中分布测压孔的方法,根据三维区中的流动特征和压力分布规律,建立压力分布与飞行参数之间的关系。试验结果表明,基于三维区理论的FADS系统得到的马赫数误差在5%左右,精度较高。
基金supported by the U.S.Department of Energy(No.DE-SC0009988)
文摘The author reviews some recent developments in Chern-Simons theory on a hyperbolic 3-manifold M with complex gauge group G. The author focuses on the case of G = SL(N, C) and M being a knot complement: M = S^3\ K. The main result presented in this note is the cluster partition function, a computational tool that uses cluster algebra techniques to evaluate the Chern-Simons path integral for G = SL(N, C). He also reviews various applications and open questions regarding the cluster partition function and some of its relation with string theory.
