全文获取类型
收费全文 | 2106篇 |
免费 | 597篇 |
国内免费 | 318篇 |
专业分类
航空 | 1749篇 |
航天技术 | 408篇 |
综合类 | 260篇 |
航天 | 604篇 |
出版年
2024年 | 19篇 |
2023年 | 44篇 |
2022年 | 125篇 |
2021年 | 112篇 |
2020年 | 107篇 |
2019年 | 99篇 |
2018年 | 98篇 |
2017年 | 118篇 |
2016年 | 76篇 |
2015年 | 122篇 |
2014年 | 115篇 |
2013年 | 143篇 |
2012年 | 182篇 |
2011年 | 186篇 |
2010年 | 182篇 |
2009年 | 184篇 |
2008年 | 170篇 |
2007年 | 169篇 |
2006年 | 162篇 |
2005年 | 110篇 |
2004年 | 100篇 |
2003年 | 60篇 |
2002年 | 69篇 |
2001年 | 62篇 |
2000年 | 54篇 |
1999年 | 42篇 |
1998年 | 30篇 |
1997年 | 17篇 |
1996年 | 10篇 |
1995年 | 6篇 |
1994年 | 5篇 |
1993年 | 15篇 |
1992年 | 5篇 |
1991年 | 5篇 |
1990年 | 4篇 |
1989年 | 4篇 |
1988年 | 2篇 |
1987年 | 4篇 |
1986年 | 2篇 |
1985年 | 2篇 |
排序方式: 共有3021条查询结果,搜索用时 15 毫秒
911.
LI Qiang FAN Wei YAN Chuan-jun HU Cheng-qi YE Bin 《中国航空学报》2007,20(1):9-14
The PDRE test model used in these experiments utilized kerosene as the fuel, oxygen as oxidizer, and nitrogen as purge gas. The solenoid valves were employed to control intermittent supplies of kerosene, oxygen and purge gas. PDRE test model was 50 mm in inner diameter by 1.2 m long. The DDT (deflagration to detonation transition) enhancement device Shchelkin spiral was used in the test model. The effects of detonation frequency on its time-averaged thrust and specific impulse were experimentally investigated. The obtained results showes that the time-averaged thrust of PDRE test model was approximately proportional to the detonation frequency. For the detonation frequency 20 Hz, the time-averaged thrust was around 107 N, and the specific impulse was around 125 s. The nozzle experiments were conducted using PDRE test model with three traditional nozzles. The experimental results obtained demonstrated that all of those nozzles could augment the thrust and specific impulse. Among those three nozzles, the convergent nozzle had the largest increased augmentation, which was approximately 18%, under the specific condition of the experiment. 相似文献
912.
913.
通过分析数控系统如何来控制机床的运动进给,构造了实现精度再生的系统模型。并将基于多体系统理论的几何误差补偿技术应用到数控系统中,开发了仿真补偿软件,达到了理想的补偿效果。 相似文献
914.
可编程信号源的软件系统由系统软件、波形监控软件和波形产生软件三大部分组成。针对该软件系统的特点,选择C 作为程序设计语言,μVision3、CCS 2000和Lab Windows/CVI作为程序开发的3个基本平台。依赖于支持C 的3个程序开发平台,设计了可编程信号源软件系统,并给出了运行结果。 相似文献
915.
916.
本文就北华航天工业学院模具设计与制造专业主干课程《塑料成型工艺及模具设计》的教学内容、教学手段、教学实训的改革进行了探讨,提出了具体的改革方案;实践表明,教学效果得到显著改善,学生不仅奠定了扎实的理论基础而且提高了实践创新能力。 相似文献
917.
本文提出了一种时间片预分割方案,并将其用于多进程实时控制系统的软件设计,其特点是程序设计简单、维护方便,尤其是提高了系统运行的可靠性。 相似文献
918.
J. Park K.W. Min V.P. Kim H. Kil H.J. Kim J.J. Lee E. Lee S.J. Kim D.Y. Lee M. Hairston 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(4):650-654
The global distribution of low-latitude plasma blobs was investigated by in-situ plasma density measurements from the Korea Multi-Purpose Satellite-1 (KOMPSAT-1) and Defense Meteorological Satellite Program (DMSP) F15. In the observations, blobs occurred in the longitude sector where the activity of the equatorial plasma bubble (EPB) was appreciable, and additional blobs were found at the lower (KOMPSAT-1) altitude as in the EPBs. However, several notable differences exist between the distributions of EPBs and blobs. First, KOMPSAT-1 found few blobs around 0°E in March and June, as did DMSP F15 from 30°W to 120°E for every season. Second, the overall occurrences in December and March at the DMSP F15 (840 km) altitude were somewhat lower than expected from those of the EBPs. Third, at the DMSP F15 altitude, the occurrence probability of plasma blobs was less controlled by yearly variations in the solar activity. These results imply that topside ionospheric conditions as well as the existence of EPBs control further development of blobs. Additionally, it was found that the blob latitudes became higher as the yearly solar activity increased. Moreover, most of the blobs were encountered in the winter hemisphere, possibly due to the low ambient density. 相似文献
919.
在线分析处理技术(OLAP)是数据仓库的重要应用之一,而安全性是许多OLAP产品的主要弱点,通过对OLAP的安全性分析,建立了OLAP的安全模型,快速、有效、安全地从数据仓库中提取有价值的信息,并以安装在Windows 2000的SQL SERVER为例,研究如何实现OLAP的安全性。 相似文献
920.
利用Pro/ENGINEER建立输入轴渐开线齿轮的模型,导入ANSYS后进行静力受载分析。结果显示,轮齿的根部应力值最大,存在危险截面,是设计和制造的着重考虑部分。 相似文献