全文获取类型
收费全文 | 5864篇 |
免费 | 824篇 |
国内免费 | 1271篇 |
专业分类
航空 | 3310篇 |
航天技术 | 1732篇 |
综合类 | 1156篇 |
航天 | 1761篇 |
出版年
2024年 | 12篇 |
2023年 | 15篇 |
2022年 | 67篇 |
2021年 | 84篇 |
2020年 | 135篇 |
2019年 | 53篇 |
2018年 | 65篇 |
2017年 | 62篇 |
2016年 | 96篇 |
2015年 | 196篇 |
2014年 | 362篇 |
2013年 | 345篇 |
2012年 | 381篇 |
2011年 | 390篇 |
2010年 | 553篇 |
2009年 | 429篇 |
2008年 | 452篇 |
2007年 | 395篇 |
2006年 | 312篇 |
2005年 | 273篇 |
2004年 | 187篇 |
2003年 | 187篇 |
2002年 | 165篇 |
2001年 | 252篇 |
2000年 | 257篇 |
1999年 | 303篇 |
1998年 | 297篇 |
1997年 | 244篇 |
1996年 | 219篇 |
1995年 | 172篇 |
1994年 | 167篇 |
1993年 | 169篇 |
1992年 | 136篇 |
1991年 | 140篇 |
1990年 | 91篇 |
1989年 | 110篇 |
1988年 | 75篇 |
1987年 | 46篇 |
1986年 | 21篇 |
1985年 | 12篇 |
1984年 | 5篇 |
1983年 | 6篇 |
1982年 | 9篇 |
1981年 | 5篇 |
1980年 | 1篇 |
1975年 | 2篇 |
1974年 | 1篇 |
1972年 | 1篇 |
1969年 | 1篇 |
1900年 | 1篇 |
排序方式: 共有7959条查询结果,搜索用时 46 毫秒
11.
12.
解决了一个计算可靠性问题的特例。分析了消旋天线机构轴承历经10年寿命试验的可靠性问题。并给出了轴承在不同可靠寿命要求下的可靠度(对应不同置信度)。 相似文献
13.
介绍一种高压快开阀装置。它可产生370MPa上升时间小于20μs的阶跃压力,用于对高压传感器进行动态校准。 相似文献
14.
黄政新 《南京航空航天大学学报》1997,29(4):365-371
杨振宁教授是位著名的物理学家,诺贝尔物理学奖金获得者。他在物理学研究中取得的成就同科学研究的艺术是分不开的。本文分析了如下三个问题:第一“对称性支配相互作用”与杨米尔斯规范场理论;第二,科学研究中的风格和taste;第三,科学研究方向的选择。该文无论是对年青的研究还是对成熟的学者从事科学研究都有指导意义。 相似文献
15.
16.
对无动力J—7LP动力学缩比模型进行了遥控试飞,以研究其失速尾旋特性,全偏平尾和方向舵可使模型进八尾旋,舵面全回中即可从各种尾旋中改出。偏转副翼对尾旋特性有明显的影响。 相似文献
17.
The architecture of digital sheet metal manufacturing system is proposed based on the classification of sheet metal manufacturing information.The essence of digital manufacturing is the definition,management and transfer of information,and the key technologies are brought forward and described.It is pointed out that knowledge-based manufacturing elements design is necessary to make digital technology efficient.The management of all kinds of sheet metal manufacturing element information is to build single source of manufacturing data.Multi-state model-based digital transfer and coordination method is designed to provide a foundation for digital manufacturing of aircraft sheet metal part.The application of digital sheet metal manufacturing is exemplified with an aircraft sheet metal part.The application result is compared to that of the traditional analog transfer technology.It is shown that the developed technology can improve part quality,shorten manufacturing time and lower manufacturing cost. 相似文献
18.
This paper proposes a neural-network current-regulated switching strategy and an intelligent controller for a matrix converter permanent magnet synchronous motor (PMSM) drive system. By using this new switching strategy, the current harmonics of the system are effectively reduced. In addition, by using the intelligent controller, position control of the drive system can be achieved and an adjustable speed range from 1 r/min to 1500 r/min can be obtained. All the current-loop, speed-loop, and position-loop control algorithms are implemented by a 32-bit TMS320C40 digital signal processor. Several experimental results are shown to validate the theoretical analysis 相似文献
19.
Liu S. Singer C.H. Dougal R.A. 《IEEE transactions on aerospace and electronic systems》2006,42(2):612-624
Electric power anomalies or disturbances can disrupt the normal operation of equipment, accelerate aging, or even cause outright failures thus resulting in increased costs of maintenance and reduced system reliability. Past research on the effects caused by power anomalies has been mostly focused on industrial, commercial, or residential systems, or on power distribution equipment. A literature survey reveals that there is no comprehensive review related to low-voltage (LV) power systems and utilization equipment applicable to military combat vehicles, such as aircraft and ships. This paper summarizes the results of a new literature survey that focused on the causes, effects, and mitigation methods for power anomalies typical of LV mobile power systems. Electric power anomaly cost data collected from the literature are also presented, from which the costs of anomalies to the national defense are estimated using some simple rationales. 相似文献
20.
The Bastille-day event in 2000 produced energetic 3B/X5.6 flare with a halo CME, which had great geo-effects consequently.
This event has been studied extensively and it is considered that it follows the two-ribbon flare model. The flare/CME event
was triggered by an erupting filament and TRACE observations showed formation of giant arcade structures during the flare
process. Hard X-ray (HXR) two ribbons revealed for the first time in this flare event (Masuda et al., 2001). The reconstruction of 3-D coronal magnetic fields revealed a magnetic flux rope structure, for the first time, from
extrapolation of observed photospheric vector magnetogram data and the flux rope structure was co-spatial with portion of
the filament and a UV bright lane (Yan et al., 2001a, 2001b). Here we review some recent work related to the flux rope structure and the HXR two ribbons by comparing their
locations and the flux temporal profiles during the flare process so as to understand the energy release and particle accelerations.
It is proposed that the rope instability may have triggered the flare event, and reconnection may occur during this process.
The drifting pulsation structure in the decimetric frequency range is considered to manifest the rope ejection, or the initial
phase of the coronal mass ejection. The HXR two ribbons were distributed along the flux rope and the rope foot points coincide
with HXR sources. The energy dissipation from IPS observations occurred within about 100 R
⋅ is consistent with the estimate for the flux rope system.
This revised version was published online in August 2006 with corrections to the Cover Date. 相似文献