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1.
研制开发了中医色诊客观化研究专用系统。该系统包括硬件和软件两部分。硬件是一个标准光源环境的图像采集装置,主要由色温为5500K的氙灯、漫反射积分球和高分辨率CCD数码相机组成。软件用于图像处理,处理过程分为3步:首先使用灰度阈值将原始图像进行肤色/非肤色分类,然后通过图像分割和坐标排序定位人脸特征,最后应用形态学技术提取与人体五脏对应的色部区域并且计算区域色度值。使用该系统采集和处理了30例年轻人和53例老年人的样本。实验结果表明年轻人和老年人色部数据有显著性差异。初步应用验证了系统在中医色诊客观化研究中的良好性能。  相似文献   
2.
采用自主研发的多源多宿GNSS-R(Global Navigation Satellite System-Reflections,全球导航卫星系统反射信号)海洋环境遥感探测系统,在天津渤海湾特定区域进行了3次机载校飞试验,获得了大量有效GNSS-R信号数据,对自然条件下的海面有效波高进行了反演处理。该系统通过对接收的GNSS直达信号和海面反射信号进行相关运算处理,可以获得DDM(Delay-Doppler Mapping,时延—多普勒映射)图谱,再利用DCF(Derivative of the Correlation Function,相关函数的导数)在DDM图谱基础上进行相关功率波形的计算,进而通过计算DCF的函数波形宽度得到海面有效波高,验证了该方法的可行性。该方法具有全天时、全天候、高分辨率、低成本等优点,对全球范围内中小尺度海洋状态和物理现象的监测具有重要意义。  相似文献   
3.
复合材料叠层板可靠度的计算方法   总被引:1,自引:0,他引:1  
羊妗 《航空学报》1988,10(10):510-513
 1.叠层板可靠度分析方法 对一般材料结构系统,美国Frcd Moses提出增量载荷法来牧举、确认结构系统的主要破坏模式和求得相应的系统强度。 飞机复合材料结构叠层板常用0°、90°、+45°和-45°4种定向层组构成,是各向异性、  相似文献   
4.
The compression creep deformation of the high volume fraction of SiC particles reinforced Al-Mg-Si composite fabricated by pressure-less infiltration was investigated. The experimental results show that the creep stress exponents are very high at temperatures of 673 K, 723 K and 773 K, and if taking the threshold stress into account, the true stress exponent of minimum creep strain rate is still approximately 5, although the volume fraction of reinforcements is very high. The creep strain rate in the high volume fraction rein- forced aluminum alloy matrix composites is controlled by matrix lattice diffusion. It is found that the creep-strengthening effect of high volume fraction of silicon carbide particles is significant, although the particles do not form effective obstacles to dislocation motion.  相似文献   
5.
空间环境对航天器影响的统计分析   总被引:2,自引:1,他引:1  
概括介绍了空间环境的九个主要区域,归纳了它们对航天器各系统的影响。对114例各类环境造成的航天器失效和异常进行了统计分析,在此基础上对引起航天器失效、异常较多的四类空间环境进行了具体分析。  相似文献   
6.
一种民用飞机结构维修大纲的制定方法   总被引:1,自引:0,他引:1  
飞机在运营之前必须制定出维修大纲。根据新研民用飞机缺少使用数据和使用经验的情况,依据类似机型结构维修大纲的制定经验,同时结合维修指导小组思想,提出案例推理的方法,制定新研机型的结构维修大纲。以案例推理为基础构建了结构维修大纲制定的方法。运用基于案例推理的方法制定出了结构维修大纲,得到结构的维修任务和维修间隔,推理结论与...  相似文献   
7.
英语修辞中有明喻、暗喻、转喻、提喻这四种常见的"喻"。它们和汉语中的明喻、暗喻、借喻、借代之间存在着相互交错的对应关系,这是导致修辞学习者时常混淆英语中"喻"的原因所在。从英语的几种常见"喻"的词源和辞格构成中可以发现,有的"喻"译称涵义偏窄,有些"喻"并非真正的比喻,其中文译称应该不含"喻"字更为合理。  相似文献   
8.
Aircraft icing has long been a plague to aviation for its serious threat to flight safety. Even though lots of methods for anti-icing have been in use or studied for quite a long time, new methods are still in great demand for both civil and military aircraft. The current study in this paper uses widely used Dielectric Barrier Discharge(DBD) plasma actuation to anti-ice on a NACA0012 airfoil model with a chord length of 53.5 cm in a closed-circuit icing wind tunnel. An actuator was installed at the leading edge of the airfoil model, and actuated by a pulsed low-temperature plasma power source. The actuator has two types of layout, a striped electrode layout and a meshy electrode layout.The ice accretion process or anti-icing process was recorded by a CCD camera and an infrared camera. Instantaneous pictures and infrared contours show that both types of DBD plasma actuators have the ability for anti-ice under a freestream velocity of 90 m/s, a static temperature of -7℃,an Median Volume droplet Diameter(MVD) of 20 lm, and an Liquid Water Content(LWC) of 0.5 g/m~3. The detected variations of temperatures with time at specific locations reveal that the temperatures oscillate for some time after spraying at first, and then tend to be nearly constant values.This shows that the key point of the anti-icing mechanism with DBD plasma actuation is to achieve a thermal equilibrium on the model surface. Besides, the power consumption in the anti-icing process was estimated in this paper by Lissajous figures measured by an oscilloscope, and it is lower than those of existing anti-icing methods. The experimental results presented in this paper indicate that the DBD plasma anti-icing method is a promising technique in the future.  相似文献   
9.
以阅读测试和调查问卷为研究工具,对广州民航职业技术学院一年级354名非英语专业学生的英语阅读策略使用情况进行定量研究,旨在为今后的阅读教学的改进提供有利信息。  相似文献   
10.
The paper summarizes research into cost-effective propulsion system options for small satellites. Research into the primary cost drivers for propulsion systems is discussed and a process for resolving them is advanced. From this analysis, a new paradigm for understanding the total cost of propulsion systems is defined that encompasses nine dimensions – mass, volume, time, power, system price, integration, logistics, safety and technical risk. This paradigm is used to characterize all near-term propulsion technology options. From this effort, hybrid rockets emerges as a promising but underdeveloped technology with great potential for cost-effective application. A dedicated research program was completed to characterize this potential. This research demonstrated that hybrid rockets offer a safe, reliable upper stage option that is a versatile, cost-effective alternative to solid rocket motors. Finally, an innovative technique was derived to parametrically combine the diverse cost dimensions into a useful, quantifiable figure of merit for mission and research planning. Overall, it is shown that the most cost-effective solution is found by weighing all options along the nine dimensions of the cost paradigm within the context of a specific mission.  相似文献   
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