全文获取类型
收费全文 | 1698篇 |
免费 | 342篇 |
国内免费 | 250篇 |
专业分类
航空 | 1538篇 |
航天技术 | 218篇 |
综合类 | 284篇 |
航天 | 250篇 |
出版年
2024年 | 5篇 |
2023年 | 21篇 |
2022年 | 59篇 |
2021年 | 77篇 |
2020年 | 96篇 |
2019年 | 96篇 |
2018年 | 66篇 |
2017年 | 95篇 |
2016年 | 107篇 |
2015年 | 108篇 |
2014年 | 120篇 |
2013年 | 117篇 |
2012年 | 127篇 |
2011年 | 141篇 |
2010年 | 126篇 |
2009年 | 111篇 |
2008年 | 87篇 |
2007年 | 94篇 |
2006年 | 83篇 |
2005年 | 75篇 |
2004年 | 56篇 |
2003年 | 46篇 |
2002年 | 52篇 |
2001年 | 35篇 |
2000年 | 32篇 |
1999年 | 23篇 |
1998年 | 25篇 |
1997年 | 34篇 |
1996年 | 30篇 |
1995年 | 21篇 |
1994年 | 22篇 |
1993年 | 19篇 |
1992年 | 26篇 |
1991年 | 11篇 |
1990年 | 15篇 |
1989年 | 16篇 |
1988年 | 10篇 |
1987年 | 4篇 |
1986年 | 2篇 |
排序方式: 共有2290条查询结果,搜索用时 578 毫秒
481.
高压液氧供应系统是我国压力最高的挤压式液体火箭发动机试验台的关键分系统。在系统设计过程中,通过合理布置管路,设计专用固定支架,采用自然补偿和堆积绝热技术,解决了高压低温推进剂系统管路设计中的难题。该系统顺利通过气密性检查和调试,经多次热试车考核,系统稳定可靠,满足设计要求。 相似文献
482.
483.
通过Ansys对单脉冲放电过程进行温度分布仿真时发现,当脉宽很小时,汽化体积所占比例很高,即材料利用率较高,但是产率较低;而加大脉宽时,产率较高,但是汽化比例较低。为综合两者的优势,利用大脉宽加工,使放电通道移动。仿真结果表明,相对于放电通道静止,其在材料利用率和产率上都有了大幅度提高。当在加工中引入高速冲液时,实验表明其能促使放电通道发生漂移,收集产物后称量、计算,其产率达到了1g/h。 相似文献
484.
针对某飞机液压系统对液压附件、部件的测试要求,设计了多支路液压系统综合试验台,实现了对飞机液压系统中作动器的动作时间、次数和速度等参数测试,对液压缸、阀、集成块等附件在不同压力、流量和温度等条件下的性能测试。该设计主要采用比例阀控制压力和流量,多级过滤器进行油源净化,PLC和继电器实现测控、电位计进行压力和流量调节,数显表直接显示压力、流量和温度、时间等参数。通过实际测试验证,试验台工作稳定、安全可靠、调整方便、显示直观、振动噪音小、不泄露,满足了某型号飞机液压附件部件测试的要求。 相似文献
485.
Masanori Matsushita Nobukatsu Okuizumi Osamu Mori Yasutaka Satou Takashi Iwasa Saburo Matunaga 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(9):2628-2642
A spinning solar sail IKAROS’s membrane is estimated to unexpectedly deform into an inverted pyramid shape due to thin-film devices with curvature, such as thin-film solar cells and steering devices on the membrane. It is important to investigate the deformation caused by the curved thin-film devices and predict the sail shape because the out-of-plane deformation greatly affects solar radiation pressure (SRP) and SRP torque. The purpose of this paper is to clarify the relationship between the global shape and orientation and position of curved thin-film devices and to evaluate SRP torque on the global shape using finite element analysis. The global shape is evaluated based on the out-of-plane displacement and the SRP torque. When the curved thin-film devices make the membrane shrink in the circumferential, diagonal, and radial direction, the sail deforms into a pyramid shape, an inverted pyramid one, and a saddle one, respectively. The saddle shape is more desirable for solar sails than the inverted pyramid shape and the pyramid one from the viewpoint of shape stability to SRP and control of SRP torque in the normal direction of the sail (windmill torque). The position of the thin-film device tends to increase the absolute value of windmill torque when it is biased circumferentially from the petal central axis. The suggested design principles for the arrangement of thin-film devices is that the curved thin-film devices should be directed so that the sail shrinks in the radial direction in order to deform the sail into a saddle shape with high shape stability, and the position of the thin-film devices should be biased in the circumferential direction paying attention to the absolute value of windmill torque to determine the direction of windmill torque. 相似文献
486.
Narcís Miguel Camilla Colombo 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(9):2561-2576
This paper studies deorbiting using an analogue to the quasi-rhombic-pyramid concept for planar motion. The focus is on maintaining a stable (meaning oscillatory) attitude close to the direction of the velocity of the spacecraft relative to the atmosphere. The study consists of a massive computation of deorbit times chosen in a region of the phase space where atmospheric drag plays a leading role. Here, no damping effects are considered. Thus, any passive stabilisation observed is either due to solar radiation pressure or atmospheric drag. The results show that such stable deorbiting is feasible up to a threshold that depends upon the physical parameters of the sail. This threshold is around 500 km of altitude. Stable deorbiting is also shown to reduce the unpredictability that appears due to tumbling. 相似文献
487.
陀螺电机转子动平衡采用的人工打孔去重存在效率低、去重精度低、金属碎屑残留等问题,严重制约了陀螺的生产效率和精度。而激光去重具有去重精度高、无接触、效率高等优点,在精密去重领域应用前景广泛。采用脉冲光纤激光器对陀螺电机转子动平衡进行了激光精密去重技术研究,探讨了激光频率、振镜扫描速度等参数对去重效果的影响规律,优化了激光去重工艺参数。当激光功率为30W、振镜扫描速度为1000mm/s时,去重盲孔效果最好。针对激光去重盲孔存在残留物问题,提出了激光二次抛光去除残留物的方法,研究了激光功率、振镜扫描速度对残留物去除效果影响规律,优化了激光抛光工艺参数。激光去重盲孔经二次扫描抛光后,盲孔表面残留物去除干净,满足陀螺电机转子的精密去重要求。 相似文献
488.
T. Azcárate B. Mendoza S. Sánchez de la Peña J.L. Martínez 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
We present a study of the temporal behavior of the systolic (SBP) and diastolic (DBP) blood pressure for a sample of 51 normotensive, healthy volunteers, 18 men and 33 women with an average age of 19 years old in Mexico City, Mexico, during April and May, 2008. We divided the data by sex along the circadian rhythm. Three geomagnetic storms occurred during the studied time-span. The strongest one, a moderate storm, is attributed to a coronal hole border that reached the Earth. The ANOVA test applied to the strongest storm showed that even though we are dealing with a moderate geomagnetic storm, there are statistically significant responses of the blood pressure. The superposed epoch analysis during a three-day window around the strongest storm shows that on average the largest changes occurred for the SBP. Moreover, the SBP largest increases occurred two days before and one day after this storm, and women are the most sensitive group as they present larger SBP and DBP average changes than men. Finally, given the small size of the sample, we cannot generalize our results. 相似文献
489.
490.
为了阐明测点布局对航空发动机进气总压畸变测试结果的影响,利用旋转总压测量耙对5种畸变流场的稳态和动态总
压畸变成分进行了测试,计算了旋转总压测量耙位于不同位置时畸变流场的稳态周向总压畸变指数和动态总压畸变指数,分析了
不同测点布局下总压畸变指数计算结果的偏差。结果表明:测量耙/测点与畸变流场的相对周向位置对总压畸变指数计算结果的
准确性至关重要,对于所分析的5种畸变流场,增加测量耙/测点周向数目并不能使总压畸变指数计算结果的偏差单调减小,但可
降低其对测量耙/测点周向位置的敏感度。基于畸变区域周向分布设计稳态总压畸变测量耙的周向位置,组合使用不同相对半径
处测点对动态总压畸变进行监测,可提高总压畸变指数计算结果的准确性。 相似文献