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401.
本文对标准的k-ε两方程模型进行了改进。摒弃了v_t=C_μ(k~2/ε)的假定,而从雷诺应力方程和Rodi的简化假设出发,得出了计算v_t的新表达式(10)。算例表明,它对时均速度u的计算结果比标准k-ε模型更精确。 相似文献
402.
Pro/ENGINEER在模具设计中的使用技巧 总被引:2,自引:0,他引:2
分析了Pro/ENGINEER进行模具设计的使用技巧,阐明了并行工程技术与Pro/ENGINEER软件相结合的重要性。 相似文献
403.
针对光学导航中存在的通过星体(球体)图像部分边缘点拟合椭圆参数计算轨道参数产生中间误差的问题,提出利用边缘点映射轨道参数的直接投影模型,避免拟合椭圆参数的方法。在小孔成像模型基础上,建立了边缘点与轨道参数的直接投影数学模型,对其映射过程进行了理论推导,利用列文伯格-马夸尔特迭代算法进行求解轨道参数。用实际探测器以及镜头参数进行数值仿真验证,结果表明:该方法在相同边缘点的条件下,轨道精度可以达到5‰。与传统方法相比,这种方法避免了椭圆的拟合过程,减少了引入中间误差过程。 相似文献
404.
Yuan Xiao Yan Su Shun Dai Jianqing Feng Shuguo Xing Chunyu Ding Chunlai Li 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2019,63(10):3404-3419
The Lunar Regolith Penetrating Radar (LRPR) is an Ultra-Wideband (UWB) array-based Ground penetrating radar (GPR) onboard the lander of Chang’e-5 (CE-5) mission. The primary scientific objectives of the LRPR are to probe the thickness and structure of lunar regolith of the landing site, and support the drilling and sampling process. In order to evaluate the performance of the LRPR, a series of ground experiments are performed using the LRPR prototype mounted on a CE-5 lander model. The performance of the LRPR is evaluated by comparing the experimental data with the simulated data. Data processing and imaging method are verified, and the interferences from the lander and other aspects are analyzed. The results of the ground experiments and simulation demonstrate that the LRPR is able to meet the design requirement of 2-m detection depth. They also indicate that the upper and lower interfaces of the stratified structure in the lunar regolith can be well distinguished by the LRPR when the dielectric constant difference is greater than 0.3, and the imaging effect of the location under the dense antennas is better than that of other positions. However, the identification capability of the LRPR to the independent blocky objects is relatively poor mainly due to the clutters caused by the lander, the sparsity of the antenna elements compared to the size of the basalt block, the limited aperture of the antenna array, and the tail of the transmitted waveform. 相似文献
405.
Jing-Fan Gao Li-Xin Guo Zheng-Wen Xu Hai-Sheng Zhao Jie Feng 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(9):2234-2244
Ionospheric inhomogeneous plasma produced by single point chemical release has simple space-time structure, and cannot impact radio wave frequencies higher than Very High Frequency (VHF) band. In order to produce more complicated ionospheric plasma perturbation structure and trigger instabilities phenomena, multiple-point chemical release scheme is presented in this paper. The effects of chemical release on low latitude ionospheric plasma are estimated by linear instability growth rate theory that high growth rate represents high irregularities, ionospheric scintillation occurrence probability and high scintillation intension in scintillation duration. The amplitude scintillations and the phase scintillations of 150?MHz, 400?MHz, and 1000?MHz are calculated based on the theory of multiple phase screen (MPS), when they propagate through the disturbed area. 相似文献
408.
It is difficult to quantitatively detect defects by using the time domain or frequency domain features of Lamb wave signals due to their dispersion and multimodal characteristics.Therefore,it is important to discover an intrinsical parameter of Lamb waves that could be used as a damage sensitive feature.In this paper,quantitative defect detection in aluminium plates is carried out by means of wavenumber analysis approach.The wavenumber of excited Lamb wave mode is a fixed value,given a frequency,a thickness and material properties of the target plate.When Lamb waves propagate to the structural discontinuity,new wavenumber components are created by abrupt wavefield change.The new wavenumber components can be identified in the frequency-wavenumber domain.To estimate spatially dependent wavenumber values,a short-space two-dimensional Fourier transform(FT)method is presented for processing wavefield data of Lamb waves.The results can be used to determine the location,size and depth of rectangular notch.The analysis techniques are demonstrated using simulation examples of an aluminium plate with a rectangular notch.Then,the wavenumber analysis method is applied to simulation data that are obtained through a range of notch depths and widths.The results are analyzed and rules of the technique with regards to estimating notch depth are determined.Based on simulation results,guidelines for using the technique are developed.Finally,experimental wavefield data are obtained in aluminium plates with rectangular notches by a full noncontact transceiving method,i.e.,laser-laser method.Band-pass filtering combined with continuous wavelet transform is used to extract a certain frequency component from the full laser-induced wavefield with wide band.Shortspace two-dimensional FT method is used for further processing full wavefield data at a certain frequency to estimate spatially dependent wavenumber values.The consistency of simulation and experimental results shows the effectiveness of proposed wavenumber method for quantitative rectangular notch detection. 相似文献
410.
Honglei Ma Feng Zhang Yu Zhu Yanhua Xiao Abrar Wazir 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
The purpose of the present study was to analyze and predict the changes in acceleration tolerance of human vertebra as a result of bone loss caused by long-term space flight. A human L3–L4 vertebra FEM model was constructed, in which the cancellous bone was separated, and surrounding ligaments were also taken into account. The simulation results demonstrated that bone loss has more of an effect on the acceleration tolerance in x-direction. The results serve to aid in the creation of new acceleration tolerance standards, ensuring astronauts return home safely after long-term space flight. This study shows that more attention should be focused on the bone degradation of crew members and to create new protective designs for space capsules in the future. 相似文献