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国家自然科学基金(10902007)

作品数:5 被引量:22H指数:2
相关作者:屈秋林郭昊刘沛清段中喆刘胜春更多>>
相关机构:北京航空航天大学国家电网公司更多>>
发文基金:国家自然科学基金国家重点基础研究发展计划更多>>
相关领域:理学电气工程环境科学与工程电子电信更多>>

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5 条 记 录,以下是 1-6
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Attractive fixed-point solution study of a shell model for turbulent convection
2013年
Different scaling behaviors, such as Kolmogorov (K41) scaling and Bolgiano and Obukhov (BO) scaling, have been reported in various shell models proposed for turbulent thermal convection. However, two coexistent subranges with K41 and BO scaling are not set up with Bolgiano scale interlaying between the largest scale and the dissipation scale. In this paper, we summarize fixed-point solution study of the Brandenburg model with small perturbation theory by introducing a small disturbance term as the impact of buoyancy. Three groups of fixed-point solutions with different locations of the so-called buoyancy scale, above/below which buoyancy is significant/insignifant. Both theoretical and numerical results show that a modified K41 scaling, instead of K41 and BO coexistent scaling, is set up even though buoyancy may be significant over the scaling range, which suggests that the buoyancy scale is not related exactly to the Bolgiano scale. Thus, a K41 and BO coexistent scaling behavior is not setup for the Brandenburg model.
GUO HaoLI ChaoQU QiuLinLIU PeiQing
关键词:湍流对流壳模型小扰动理论
Generation of spatial atmospheric turbulence field in aircraft motion simulation based on refined similarity hypothesis被引量:1
2011年
It is necessary to build turbulence model to study the response of aircraft to atmospheric turbulence for high resolution earth observation. The conventional method is on the basis of Dryden’s model with the assumption that individual patches are Gaussian. In this paper,based on Kraichnan’s refined similarity idea,a new 1D atmospheric turbulence model is set up by introducing the energy transfer rate as an intermittency disturbance to a Gaussian process. Our results show that the turbulent fields generated by our new method exhibit an anomalous scaling described by the She-Leveque (SL) formula,which is now well accepted for homogenous and isotropic turbulence.
GUO Hao CHEN JingJing QU QiuLin LIU PeiQing
关键词:大气湍流空间飞行器均匀各向同性湍流对地观测
输电线雾凇覆冰的工程估算方法被引量:16
2011年
为克服目前输电线覆冰数学模型存在各种上缺陷的问题,利用输电线雾凇覆冰的数值模拟方法系统探讨了输电线覆冰过程中过冷却水滴撞击输电线表面的碰撞特性,分析总结了各碰撞特性参数之间的相互依赖关系并导出了简单有效的碰撞特性估算公式,分析结果表明,水滴与筒状物的总碰撞率可由Finstad经验公式描述,局部碰撞率沿冰面为抛物线分布。在碰撞特性估算公式基础上分别给出不同状态下输电线雾凇覆冰的工程估算方法,估算结果表明,圆筒状雾凇覆冰估算工程模型结果与实验结果比较相符,表明估算方法正确有效;固定导线雾凇覆冰工程估算方法结果与数据模拟结果相较,覆冰质量估算的误差较小,但覆冰外形有一定的差别,需要进一步改进外形估算方法。
郭昊刘沛清屈秋林段中喆
关键词:数值模拟
输电线雾凇覆冰过程的二维数值模拟被引量:6
2011年
基于拉格朗日法提出了一种输电线表面雾凇覆冰过程的二维数值模拟方法。采用同位网格上的SIMPLE算法求解非定常不可压缩流动的RANS方程和SST-k-ω湍流模型以获得空气流场;采取拉格朗日法跟踪流场中过冷水滴的运动轨迹得到输电线表面各控制体的瞬时局部碰撞率;求解基于Messinger控制容积法建立的覆冰热力学方程以获得各控制体的雾凇覆冰温度,并结合覆冰时间推进法模拟覆冰过程。研究结果表明,预测的冰形与文献中的实验测量数据吻合较好,证明该文的方法是可行和有效的。
郭昊刘沛清屈秋林刘胜春王景朝邸玉贤
关键词:数值模拟
Attractive fixed-point solution study of shell model for homogeneous isotropic turbulence
2013年
The attractive fixed-point solution of a nonlinear cascade model is studied for the homogeneous isotropic turbulence containing a parameter C, introduced by Desnyansky and Novikov. With a traditional constant positive external force added on the first shell equation, it can be found that the attractive fixed-point solution of the model depends on both the parameter C and the external force. Thus, an explicit force is introduced to remove the effects of the external force on the attractive fixed-point solution. Furthermore, two groups of attractive fixed-point solutions are derived theoretically and studied numerically. One of the groups has the same scaling behavior of the velocity in the whole inertial range and agrees well with those observed by Bell and Nelkin for the nonnegative parameters. The other is found to have different scaling behaviors of the velocity at the odd and even number shells for the negative parameters. This special characteristic may be used to study the anomalous scaling behavior of the turbulence.
郭昊李超屈秋林刘沛清
关键词:各向同性湍流壳模型IED
A Research on the Aircraft’s Six Degree of Freedom Flight Dynamics Modeling and Simulation under Atmospheric Turbulence
Taking a certain type of aircraft as example, this paper builds a six degree of freedom motion equation model ...
Qu Zukun
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