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191.
在雷诺数8.7×10^5的条件下,运用眼镜蛇探针、压力扫描阀和表面油膜流动可视化技术对倾角为25°的Ahmed类车体尾流与尾部压力分布进行了研究。对比了模型尾部斜面上边缘和两侧不同宽度导流板对模型尾流与气动阻力的影响规律。实验发现模型尾流中存在一对对称的拖曳涡,其在尾流中心线附近形成强烈的下扫流。拖曳涡强度与模型尾部压力分布和气动阻力有直接关系,较强的拖曳涡对应的模型尾部负压以及气动阻力均较大。斜面两侧导流板宽度为1%模型长度时,不仅无减阻效果,反而会使气动阻力增加约3.0%。当导流板宽度增加为2%和3%模型长度时,能够明显削弱斜面上的分离泡,对应的减阻效果分别为3.5%和7.2%。斜面上边缘导流板可有效地抑制分离流在斜面上的再附,并消除斜面上的分离泡,其抑制拖曳涡强度和降低气动阻力的效果明显优于同等宽度的斜面两侧导流板。上边缘导流板宽度为模型长度的1%,2%和3%时,减阻率分别可达9.3%,10.7%和10.9%。 相似文献
192.
基于非结构动网格的非定常激波装配法 总被引:5,自引:0,他引:5
从ALE方程出发,通过修正体积的新思路构建离散几何守恒律,基于非结构动网格的信息传递方法得到网格重构以后新网格的流场参数,采用一阶格式捕捉法得到的流场确定装配法的初始激波位置,成功地把激波装配法应用到非定常流动的模拟。模拟超声速飞行环境下整流罩分离的非定常流固耦合过程,在马赫数6条件下装配法和捕捉法的计算结果完全一致,随着马赫数增加,二阶精度格式的捕捉法需要进行调整限制器参数、时间步长等人工干预,但是装配法直到马赫数20计算过程没有出现异常。该基于非结构动网格技术的激波装配方法,与传统的激波装配方法相比,能够用于复杂外形产生的非规则形状激波和非定常流动产生的运动激波,解决二阶精度有限体积法用于高马赫数飞行条件下多体分离过程的流动模拟时遇到的稳定性问题。 相似文献
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195.
非系统RS码的删/错译码算法 总被引:1,自引:0,他引:1
邹世开 《北京航空航天大学学报》1990,(1):81-87
研究了非系统RS码的删/错译码算法。详细阐明了删/错译码原理,推导了各步的计算公式。该算法特别适用于干扰严重的组合信道中级连RS码的译码。 相似文献
196.
Yongchao Zhu Yongchun Zheng Shibo Fang Yongliao Zou Simon Pearson 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2019,63(1):750-765
Compared with other remote observations, brightness temperatures (TB) derived from microwave emission measurements provide a unique means to characterize the physical properties of the lunar surface. Using Chang’E-2 microwave radiometer data, we produced 12 global TB images of the lunar surface during a diurnal cycle with different local times separated by approximately 2?h. There are two types of remarkable TB units on the lunar surface, the “hot regions” occurring during the lunar day in the lunar Maria regions and the “microwave cold spots” occurring during the nighttime typically related to young craters. Compared with their surroundings, the hot regions are much warmer during the lunar day and slightly colder at night, while the microwave cold spots are much colder during the lunar night and slightly warmer in the daytime. Moreover, the TB heating and cooling rates of these two units are larger than others at the same average latitude where they are located during the lunar day, especially after sunrise and before sunset. The hot regions have a good agreement with the mare regions with high TiO2 abundance. Besides, brightness temperatures in the lunar Maria correlate closely with their TiO2 abundance. For most microwave cold spots, they agree with the young craters, and their brightness temperature distributions have a significant negative correlation with the lunar surface nighttime temperature and rock abundance. 相似文献
197.
Yang Zhang Binbin Ni Zheng Xiang Xianguo Zhang Xiaoxin Zhang Xudong Gu Song Fu Xing Cao Zhengyang Zou 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(9):2290-2300
We perform an L-shell dependent inter-satellite calibration of FengYun 3 medium energy electron measurements with POES measurements based on rough orbital conjunctions within 5?min?×?0.1?L?×?0.5 MLT. By comparing electron flux data between the U.S. Polar Orbiting Environmental Satellites (POES) and Chinese sun-synchronous satellites including FY-3B and FY-3C for a whole year of 2014, we attempt to remove less reliable data and evaluate systematic uncertainties associated with the FY-3B and FY-3C datasets, expecting to quantify the inter-satellite calibration factors for the 150–350?keV energy channel at L?=?2–7. Compared to the POES data, the FY-3B and FY-3C data generally exhibit a similar trend of electron flux variations but more or less underestimate them within a factor of 5 for the medium electron energy 150–350?keV channel. Good consistency in the flux conjunctions after the inter-calibration procedures gives us certain confidence to generalize our method to calibrate electron flux measurements from various satellite instruments. 相似文献
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199.
This work aims to investigate local stress distribution, damage evolution and failure of notched composite laminates under in-plane loads. An analytic method containing uniformed boundary equations using a complex variable approach is developed to present layer-by-layer stresses around the notch. The uniformed boundary equations established in series together with conformal mapping functions are capable of dealing with irregular boundary issues around the notch and at infinity. Stress results are employed to evaluate the damage initiation and propagation of notched composites by progressive damage analysis(PDA). A user-defined subroutine is developed in the finite element(FE) model based on coupling theories for mixed failure criteria and damage mechanics to efficiently investigate damage evolution as well as failure modes. Carbon/epoxy laminates with a stacking sequence of [45°/0°/ 60°/90°]sare used to investigate surface strains, in-plane load capacity and microstructure of failure zones to provide analytic and FE methods with strong validation. Good agreement is observed between the analytic method, the FE model and experiments in terms of the stress(strain) distributions, damage evaluation and ultimate strength, and the layerby-layer stress components vary according to a combination effect of fiber orientation and loading type, causing diverse failure modes in individuals. 相似文献
200.
粉末锻造钢12Cr2Ni4A和18Cr2Ni4WA的组织与性能 总被引:1,自引:0,他引:1
讨论了粉末锻造钢12Cr2Ni4A和18Cr2Ni4WA的组织与性能。氧含量低于0.2%,碳含量为0.08~0.12%的粉末锻造钢12Cr2Ni4A和碳含量为0.11~0.16%的粉末锻造钢18Cr2Ni4WA有较好的力学性能。长时间扩散退火可有效地提高粉末锻造钢的韧性。 相似文献