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101.
本文针对航天飞机机翼前缘的简化模型,即楔-后掠柱模型,在大后掠、高超声速条件下,提供了一种计算柱体前缘激波干扰流场和热流的工程计算方法。在中国科技大学流体力学实验室的激波风洞中取得了激波干扰的流场显示结果。计算的结果与国内外实验数据的比较表明,这是一种有效的方法。 相似文献
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对太阳系尘埃动力学所涉及到的基本内容进行概述,包括尘埃的种类、成分、尺寸、密度、形状和生命周期。介绍了近年来在尘埃的来源与生成机制方面的力学过程、主要理论、模型与方法,包括冲击溅射、表面喷射、风化、滑坡、质量脱落、旋转断裂等,阐述了尘埃的充电过程与磁场环境,简要概述了航天任务的尘埃探测结果,介绍了尘埃受力模型、单个尘埃颗粒的运动以及大量尘埃的分布特征、动力学现象及内在规律方面的最新研究结论。最后对太阳系尘埃动力学领域的未来发展趋势进行了展望。 相似文献
104.
R. Spang L. Hoffmann A. Kullmann F. Olschewski P. Preusse P. Knieling S. Schroeder F. Stroh K. Weigel M. Riese 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008
The Cryogenic Infrared Spectrometers and Telescopes for the Atmosphere – New Frontiers (CRISTA-NF) experiment on board the Russian research aircraft Geophysica measures limb emission spectra with an unprecedented vertical and horizontal resolution in the 4–15 μm wavelength region. The IR spectra measured during the SCOUT-O3 Tropical Aircraft Campaign have been analysed with respect of cloud occurrence, cloud vertical and horizontal extent, cloud spatial structures and their utilisation for trace gas retrievals. In addition indicators for ice water content and optical thickness of the clouds have been adopted. These new kinds of measurements in the upper troposphere/lower stratosphere region are especially valuable for the design and development of future space borne high resolution limb sounders. 相似文献
105.
大型结冰风洞云雾场适航应用符合性验证 总被引:2,自引:0,他引:2
结冰风洞云雾场符合性是大型结冰风洞适航应用的基础。为验证3 m×2 m结冰风洞云雾场符合性,发展了基于SAE ARP5905的结冰风洞云雾场符合性验证方法,针对主试验段构型,开展了结冰云雾场符合性验证试验,获得了试验段内液滴尺寸和液态水含量拟合关系,考察了喷嘴水压、液滴尺寸、试验段气流速度和喷嘴数量对试验段液态水含量的影响,形成了主试验段结冰云雾控制包线。结果表明:主试验段内液滴尺寸分布具有显著的单峰分布特征,体积中值直径(MVD)模拟范围近似在10~75 μm之间;试验段中心处液态水含量随着喷嘴水压和MVD的增大而增大,同时近似与试验段气流速度成反比,与喷嘴数量成正比;增大喷嘴水压和喷嘴数量会提高试验段内云雾液态水含量空间均匀性,但是增大气流速度却会减弱试验段内云雾空间均匀性;3 m×2 m结冰风洞主试验段结冰云雾控制包线可以覆盖大部分适航条例25部附录C结冰气象条件,但对低液态水含量结冰条件的模拟仍存在局限。 相似文献
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107.
Xiyao Huang Xiangyuan Zeng Christian Circi Giovanni Vulpetti Dong Qiao 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(9):2613-2627
The deformation of the solar-sail membrane is an important factor for causing inaccuracies in the solar-sail missions. This paper describes the solar sail under deformation by using a new modelling technique based on point cloud and triangular mesh generation. Two types of deformation, stemming from wrinkling and billowing, are modelled. The changes in the solar radiation pressure force and the moment caused by deformation are calculated and compared to the ideal non-deformed case. The heliocentric spiral trajectory and the orbital angular momentum reversal trajectory are taken as examples to quantify the influence of the deformation from an orbit point of view. Additionally, point cloud simplification, based on the normal vector and bounding box, is utilized to simplify the original deformed-sail model. It involves a reasonable reduction and renewal of the points in the model considering the variation of surface curvature. The simplification and its modelling accuracy are numerically investigated as well as computational efficiency. 相似文献
108.
Objective and accurate classification model or method of cloud image is a prerequisite for accurate weather monitoring and forecast. Thus safety of aircraft taking off and landing and air flight can be guaranteed. Thresholding is a kind of simple and effective method of cloud classification. It can realize automated ground-based cloud detection and cloudage observation. The existing segmentation methods based on fixed threshold and single threshold cannot achieve good segmentation effect. Thus it is difficult to obtain the accurate result of cloud detection and cloudage observation. In view of the above-mentioned problems, multi-thresholding methods of ground-based cloud based on exponential entropy/exponential gray entropy and uniform searching particle swarm optimization (UPSO) are proposed. Exponential entropy and exponential gray entropy make up for the defects of undefined value and zero value in Shannon entropy. In addition, exponential gray entropy reflects the relative uniformity of gray levels within the cloud cluster and background cluster. Cloud regions and background regions of different gray level ranges can be distinguished more precisely using the multi-thresholding strategy. In order to reduce computational complexity of original exhaustive algorithm for multi-threshold selection, the UPSO algorithm is adopted. It can find the optimal thresholds quickly and accurately. As a result, the real-time processing of segmentation of groundbased cloud image can be realized. The experimental results show that, in comparison with the existing groundbased cloud image segmentation methods and multi-thresholding method based on maximum Shannon entropy, the proposed methods can extract the boundary shape, textures and details feature of cloud more clearly. Therefore, the accuracies of cloudage detection and morphology classification for ground-based cloud are both improved. 相似文献
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110.
虽然针对互击式气-液喷注器开展了大量研究,但对互击式气-气喷注器的了解甚少。为了深入理解互击式气-气喷注器气气混合过程的特点,利用粒子图像测速(PIV)系统对其开展了流动显示实验研究。实验结果表明:对于O-F-O互击式气-气喷注器,气流撞击角度和氧/氢动量比直接影响着气流撞击作用的大小,控制着气流混合过程;对于喷孔间距保持一定时,撞击角越大,气流间的相互作用越强,气流混和效果越好;氧/氢动量比越大,气流间撞击力越强,混合距离越短,对中心气流的挤压作用越厉害,其流场分布三维特征越明显;可以通过组合高的氧压降、低的氢压降和大撞击角来设计混合效果较好的互击式气-气喷注器。 相似文献