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121.
《中国航空学报》2021,34(12):227-237
A study of composite laminates under tension–torsion biaxial loading is presented. The focus is placed on fatigue lives of composite laminates under different tension–torsion biaxial fatigue loading paths. A macro-meso model used to predict multiaxial fatigue life of composite laminates is also presented in this paper. Firstly, a macro-scale 3D RVE corresponding to composite laminates is established to determine strain components in the material principal direction of each layer for each biaxial stress ratio. Secondly, a meso-scale 3D RVE corresponding to each layer with fibers distributed randomly is established, with progressive damage prediction method, biaxial strength of composite laminates can be predicted, and the final failure layer can be confirmed. Thirdly, select any one of fatigue loading path at which the final failure of composite laminates is fiber failure (matrix failure) to establish the reference curve for fiber (matrix). Finally, with reference curve, fatigue life of composite laminates under any biaxial loading path can be predicted. And numerical results show good agreements with experimental data. 相似文献
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123.
Jonathan G. Metts James A. Nabity David M. Klaus 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
Variable emissivity electrochromics have been proposed as an enabling technology for integrating a radiator capability into a space suit in order to augment or replace the traditional means of heat rejection achieved via water sublimation. Thermal analysis was performed to establish design trade spaces and to provide operational guidelines and performance specifications for electrochromic technology development. Based on using the available surface area of an entire space suit as a radiator and the projected infrared emissivity modulation capability of state-of-the-art electrochromic material, the proposed application for space suit heat rejection suggests the potential exists to reduce or eliminate reliance on water consumption for thermal control within a defined range of metabolic and environmental boundary conditions. 相似文献
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125.
初始气孔率热老化试验研究与应用:预测双基推进剂储存寿命的一种新方法 总被引:1,自引:0,他引:1
通过对双基推进剂药柱进行初始气孔率热老化试验研究。探讨了用累积损伤理论和粘弹性分析方法来预测药柱储存寿命的理论基础和应用价值,提出了一种准确,经济,方便的预测药柱储存寿命的新方法。 相似文献
126.
分析了引起复合材料舱体软木粘贴质量问题的原因。按GD414和717胶的技术条件要求,对HYJ-51、J-48胶与GD414、717胶进行对比,选用HYJ-51胶并进行工艺适用性改进,如延长胶粘剂适用期等。探索了口框局部缺陷修补方法、基材表面处理、加压方式。通过软木粘贴工艺的改进,提高了口盖与口框的装配质量、软木粘贴质量、软木外表面涂层附着质量。 相似文献
127.
中国返回式卫星的搭载任务—空间生命科学试验 总被引:8,自引:0,他引:8
自1987年以来,为充分利用中国返回式卫星的剩余载荷能力,有计划地以搭载形式进行了一系列空间科学和技术试验,取得了较好的效果,文章简要介绍了在空间生命科学试验方面取得的成果。 相似文献
128.
灰色可靠性分析及其应用的研究 总被引:4,自引:0,他引:4
本文从可靠性技术出发,结合灰色系统的概念,对结构工程强度和寿命最佳设计问题,提出了灰色可靠性分析,有其实用价值,可供参考。 相似文献
129.
新一代箭载无线传感器网络系统架构综述 总被引:2,自引:0,他引:2
无线传感器网络技术是新一代火箭测量系统中的关键技术之一。在简要介绍现有箭载无线传感器网络应用的基础上,分析归纳了各个现有系统的技术特点,并以此提出了新一代箭载无线传感器网络的系统架构EPSEN,其中对通信协议的设计思路进行了详细阐述。EPSEN架构的提出,为现有箭载无线传感器网络系统的改进和未来产品的研制提供了重要参考依据,有助于行业标准的形成。 相似文献
130.
M. Nelson W.F. Dempster J.P. Allen S. Silverstone A. Alling M. van Thillo 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(5):748-753
An experiment utilizing cowpeas (Vigna unguiculata L.), pinto beans (Phaseolus vulgaris L.) and Apogee ultra-dwarf wheat (Triticum sativa L.) was conducted in the soil-based closed ecological facility, Laboratory Biosphere, from February to May 2005. The lighting regime was 13 h light/11 h dark at a light intensity of 960 μmol m−2 s−1, 45 mol m−2 day−1 supplied by high-pressure sodium lamps. The pinto beans and cowpeas were grown at two different planting densities. Pinto bean production was 341.5 g dry seed m−2 (5.42 g m−2 day−1) and 579.5 dry seed m−2 (9.20 g m−2 day−1) at planted densities of 32.5 plants m−2 and 37.5 plants m−2, respectively. Cowpea yielded 187.9 g dry seed m−2 (2.21 g m−2 day−1) and 348.8 dry seed m−2 (4.10 g m−2 day−1) at planted densities of 20.8 plants m−2 and 27.7 plants m−2, respectively. The crop was grown at elevated atmospheric carbon dioxide levels, with levels ranging from 300–3000 ppm daily during the majority of the crop cycle. During early stages (first 10 days) of the crop, CO2 was allowed to rise to 7860 ppm while soil respiration dominated, and then was brought down by plant photosynthesis. CO2 was injected 27 times during days 29–71 to replenish CO2 used by the crop during photosynthesis. Temperature regime was 24–28 °C day/deg 20–24 °C night. Pinto bean matured and was harvested 20 days earlier than is typical for this variety, while the cowpea, which had trouble establishing, took 25 days more for harvest than typical for this variety. Productivity and atmospheric dynamic results of these studies contribute toward the design of an envisioned ground-based test bed prototype Mars base. 相似文献