检索规则说明:AND代表“并且”;OR代表“或者”;NOT代表“不包含”;(注意必须大写,运算符两边需空一格)
检 索 范 例 :范例一: (K=图书馆学 OR K=情报学) AND A=范并思 范例二:J=计算机应用与软件 AND (U=C++ OR U=Basic) NOT M=Visual
作 者:陈勇[1] 路大举[2] 谢伟明[1] 姚向红[1] 袁强[1] 吴运刚[1] Chen Yong;Lu Daju;Xie Weiming;Yao Xianghong;Yuan Qiang;Wu Yungang(Facility Design and Instrumentation Institute,China Aerodynamics Research and Development Center,P.O.Box 12-04,Mianyang 621000,China;Institute of Applied Electronics,CAEP,P.O.Box 919-1012,Mianyang 621900,China)
机构地区:[1]中国空气动力研究与发展中心设备设计及测试技术研究所,四川绵阳621000 [2]中国工程物理研究院应用电子学研究所,四川绵阳621900
出 处:《强激光与粒子束》2020年第8期1-5,共5页High Power Laser and Particle Beams
摘 要:采用耦合J-B模型的IDDES模型与双时间步LU-SGS方法开展炮塔非稳态气动载荷的数值仿真研究。炮塔流动会发生分离,天顶位置的分离角大于90°;当流动绕过炮塔时,形成马蹄涡、脱落涡街等非稳态流场结构,导致气动载荷也具有非稳态特性;炮塔顶点的脉动静压功率谱在1.6~40.0 kHz进入各向同性均匀湍流的惯性子区,基本满足Kolmogrov的-5/3定律;气动力以阻力为主,横向力的脉动幅值大,气动力矩则以俯仰力矩为主,滚转力矩的脉动幅值大,偏航力矩可以忽略不计;气动力和力矩的功率谱主要集中在1 kHz以下,存在多个尖峰频率,主频约为230 Hz (斯特劳哈尔数为0.15)。在ATP系统设计之初,需要考虑光学炮塔所受气动载荷的非稳态特性,并规避尖峰频率尤其是主频的谐振破坏问题。IDDES coupled with J-B model and dual time step LU-SGS method has been adopted to carry out numerical simulation research on unsteady aerodynamic loads on a turret. Flow around the turret will separate, and the separation angle at the zenith is greater than 90°. When the flow bypasses the turret, unsteady flow field structures such as horseshoe vortex and shedding vortex street will form, resulting in unsteady aerodynamic loads. Power spectral density of pulsating static pressure at the zenith lies in the inertial sub-region of isotropic and uniform turbulence at 1.6-40.0 kHz, which basically satisfies Kolmogrov’s-5/3 law. Aerodynamic force is mainly drag force,fluctuation amplitude of transverse force is large, while aerodynamic moment is mainly pitching moment, fluctuation amplitude of rolling moment is also large, but yaw moment can be ignored. The power spectra of aerodynamic force and moment are mainly concentrated below 1 kHz, there are obvious peak frequencies, and the dominant frequency is about 230 Hz(Strouhal number is 0.15). At the beginning of the design of the acquisition tracking pointing(ATP)system, unsteady characteristics of aerodynamic loads on the turret should be considered, and resonant failure problem caused by peak frequencies, especially the dominant frequency, should be avoided.
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在链接到云南高校图书馆文献保障联盟下载...
云南高校图书馆联盟文献共享服务平台 版权所有©
您的IP:3.129.250.3