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131.
针对起伏海面高频声散射计算问题,提出了一种改进的基尔霍夫(Kirchhoff)近似方法。该方法考虑了海面的阴影区和亮区之间的多次散射声场,可对小入射角下大粗糙度起伏海面的散射声场进行计算。以一维余弦和高斯谱海面散射声场的有限元计算结果为标准解验证了所提方法的准确性和适用性。利用该方法计算了一维余弦海面的散射强度,分析了不同入射声波频率和角度下海面散射强度的分布情况,并解释了Bragg散射的产生机理,同时讨论了不同海面均方根高度和相关长度情况下高斯谱海面散射强度的变化规律。 相似文献
132.
作为微电子器件中最具发展前景的高介电薄膜材料,HfO2薄膜得到了学者们的广泛研究。低漏电流是HfO2薄膜使器件获得优良性能的前提,但易受晶粒尺寸、氧空位和粗糙度等因素影响。针对反应磁控溅射所得薄膜表面粗糙度高及漏电流密度大等缺点,本文在溅射过程中通过在衬底施加偏压的方法降低了HfO2薄膜的漏电流密度。结果表明:通过在衬底施加适当的偏压使得Y掺杂HfO2(Y∶HfO2)薄膜的漏电流密度降低到8×10-8 A/cm2。漏电流密度的变化与薄膜粗糙度和晶粒尺寸有关,而薄膜粗糙度和晶粒尺寸主要受衬底偏压的影响,但衬底偏压对薄膜物相的影响可以忽略。通过施加衬底偏压,利用反应磁控溅射方法制备了低漏电流和高k值Y∶HfO2薄膜,可为高性能器件的制备提供基础。 相似文献
133.
Sanghwan Choi Eungchul Kim Hyunho Seok Taesung Kim 《Advanced Engineering Materials》2023,25(16):2370055
Polycrystalline silicon (poly-Si) is widely used as a gate layer in integrated circuits, transistors, and channels through nanofabrication. Nanoremoval and roughness control are required for nanomanufacturing of various electronic devices. Herein, a nanoscale removal method is developed to overcome the limitations of microcracks, complex procedures, and time-consuming conventional fabrication and lithography methods. The method is implemented with a mechanically induced poly-Si phase transition using atomic force microscope (AFM). Mechanical force induces the covalent bonds between silicon and fluorine atoms which cause the phase transition of poly-Si. Then, the bond structure of the Si molecules is weakened and selectively removed by nano-Newton-scale force using AFM. A selective nanoscale removal with roughness control is implemented in 0.5 mM TBAF solution after mechanical force (43.58–58.21 nN) is applied. By the magnitude of nano-Newton force, the removal depth of poly-Si is controlled from 2.66 to 21.52 nm. Finally, the nanoscale fabrication on poly-Si wafer is achieved. The proposed nanoremoval mechanism is a simple fabrication method that provides selective, nanoscale, and highly efficient removal with roughness control. 相似文献
134.
Current wind erosion and dust emission models neglect the heterogeneous nature of surface roughness and its geometric anisotropic effect on aerodynamic resistance, and over-estimate the erodible area by assuming it is not covered by roughness elements. We address these shortfalls with a new model which estimates aerodynamic roughness length (z0) using angular reflectance of a rough surface. The new model is proportional to the frontal area index, directional, and represents the geometric anisotropy of z0. The model explained most of the variation in two sets of wind tunnel measurements of aerodynamic roughness lengths (z0). Field estimates of z0 for varying wind directions were similar to predictions made by the new model. The model was used to estimate the erodible area exposed to abrasion by saltating particles. Vertically integrated horizontal flux (Fh) was calculated using the area not covered by non-erodible hemispheres; the approach embodied in dust emission models. Under the same model conditions, Fh estimated using the new model was up to 85% smaller than that using the conventional area not covered. These Fh simulations imply that wind erosion and dust emission models without geometric anisotropic sheltering of the surface, may considerably over-estimate Fh and hence the amount of dust emission. The new model provides a straightforward method to estimate aerodynamic resistance with the potential to improve the accuracy of wind erosion and dust emission models, a measure that can be retrieved using bi-directional reflectance models from angular satellite sensors, and an alternative to notoriously unreliable field estimates of z0 and their extrapolations across landform scales. 相似文献
135.
程俊 《数字社区&智能家居》2011,(5):1164-1165
Multisim10是原理电路设计、电路功能测试的仿真软件.该文利用Multisim10对高频电路中的功率放大器和正弦波振荡器进行了分析,其结果符合理论推导.将Multisim10引入到高频实验教学中,不但能提高学生的学习兴趣,帮助学生更好理解原理电路以及相关特性的测试方法,而且还能提高学生的电路设计能力. 相似文献
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This paper investigates robust observer‐controller compensator design using Vidyasagar's structure (VS). VS has a unit matrix parameter H similar to the Q parameter for the Youla–Kucera parameterization. VS can be designed based on the left coprimeness of the central controller in the H∞‐loop shaping design procedure (H∞‐LSDP) and therefore can preserve the intrinsic properties of the H∞‐LSDP. This paper introduces algebraic methods to simplify the design of H in the VS controller by solving specific algebraic equations. In particular, the algebraic design of H can achieve two things. First, a dynamic H adjusts the tracking performance and yields the integral action. Second, a dynamic H rejects the input and output sinusoidal disturbances with known frequencies. These attributes are indications of the flexibility of the proposed method since the output‐feedback controller design of the H∞‐LSDP cannot easily deal with such conditions. This paper discusses the achieved loop and the closed‐loop behavior of the system with VS, and also gives two numerical examples. The first example shows that the proposed method results in a better design in many aspects than the resulting from H∞‐LSDP. The second example shows the application of the proposed method to rejecting input and output step disturbances, and input and output multiple sinusoidal disturbances, for which the H∞‐LSDP can hardly be used. Copyright © 2009 John Wiley & Sons, Ltd. 相似文献
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