全文获取类型
收费全文 | 91篇 |
免费 | 57篇 |
国内免费 | 21篇 |
专业分类
航空 | 114篇 |
航天技术 | 14篇 |
综合类 | 6篇 |
航天 | 35篇 |
出版年
2024年 | 2篇 |
2023年 | 2篇 |
2022年 | 12篇 |
2021年 | 6篇 |
2020年 | 9篇 |
2019年 | 6篇 |
2018年 | 2篇 |
2017年 | 14篇 |
2016年 | 7篇 |
2015年 | 3篇 |
2014年 | 9篇 |
2013年 | 6篇 |
2012年 | 8篇 |
2011年 | 7篇 |
2010年 | 5篇 |
2009年 | 9篇 |
2008年 | 12篇 |
2007年 | 1篇 |
2006年 | 8篇 |
2005年 | 3篇 |
2004年 | 6篇 |
2003年 | 3篇 |
2002年 | 5篇 |
2001年 | 4篇 |
2000年 | 1篇 |
1999年 | 1篇 |
1998年 | 3篇 |
1997年 | 2篇 |
1996年 | 3篇 |
1995年 | 2篇 |
1994年 | 2篇 |
1993年 | 5篇 |
1992年 | 1篇 |
排序方式: 共有169条查询结果,搜索用时 15 毫秒
91.
GaAs太阳电池在空间辐射条件下的性能衰减与电池内部微观结构紧密相关。文章针对空间辐射带质子辐照GaAs材料,利用分子动力学方法研究由被辐射材料中产生的不同能量(0.1~10 ke V)初级离位原子(PKA)引起的级联碰撞过程,分析缺陷随辐照时间、入射PKA能量的演化规律,探讨点缺陷和缺陷簇的形成特征。研究发现,在GaAs材料的缺陷对数目随时间的演化曲线中,在"离位峰"和稳定状态时,缺陷对数目与PKA能量呈一定的线性关系;PKA能量越高,辐射损伤越严重、越不易恢复,但缺陷复合率随能量升高趋于饱和;点缺陷在GaAs中主要以缺陷簇的方式存在,且随着能量的升高,孤立缺陷倾向于缔合成缺陷簇。 相似文献
92.
93.
The start-up current control of the high-speed brushless DC (HS-BLDC) motor is a chal-lenging research topic. To effectively control the start-up current of the sensorless HS-BLDC motor, an adaptive control method is proposed based on the adaptive neural network (ANN) inverse system and the two degrees of freedom (2-DOF) internal model controller (IMC). The HS-BLDC motor is identified by the online least squares support vector machine (OLS-SVM) algo-rithm to regulate the ANN inverse controller parameters in real time. A pseudo linear system is developed by introducing the constructed real-time inverse system into the original HS-BLDC motor system. Based on the characteristics of the pseudo linear system, an extra closed-loop feed-back control strategy based on the 2-DOF IMC is proposed to improve the transient response per-formance and enhance the stability of the control system. The simulation and experimental results show that the proposed control method is effective and perfect start-up current tracking perfor-mance is achieved. 相似文献
94.
M.V. Klimenko V.V. Klimenko I.E. Zakharenkova S.A. Pulinets B. Zhao M.N. Tsidilina 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
The problems of physical explanation and possible mechanisms of the seismo-ionospheric effects formation are under discussion now. There are proposed different mechanisms of such effects, for example, large- and small-scale internal gravity waves (IGWs), atmospheric electric field, electromagnetic fields and emissions. However, the appearance of local large-scale seismo-ionospheric anomalies in Total Electron Content (TEC) is possible to explain only by two mechanisms: an atmospheric electric field and/or small-scale IGWs. In this paper, the simulation results for reproduction of the observed seismo-ionospheric great positive effects in TEC prior to strong Wenchuan earthquake are presented. The obtained results confirm the proposed mechanism of seismo-ionospheric effects formation by the penetration of the seismogenic electric field from the atmosphere into the ionosphere. It is suggested that so great TEC enhancement observed 3 days prior to Wenchuan earthquake could be explained by combined action of seismogenic vertical electric field and IGWs generated by the solar terminator. 相似文献
95.
96.
当前AutoCAD的图形输出存在着很多对外不公开文件格式,为实现加工信息的集成及数控加工,必须对AutoCAD的图形文件进行访问、读取、转化成我们所需要的格式,所以对访问AutoCAD图形文件的方法必须进行深入分析,详细地论述访问AutoCAD的图形文件的LISP、VBA、DXF、Ob jectX ARX等各种方法的优缺点,从而可根据不同的开发环境,选择合适的开发方法,以提高工作效率。 相似文献
97.
This paper considers a spinning rigid body and a particle with internal motion under axial thrust. This model is helpful for gaining insights into the nutation anomalies that occurred near the end of orbit injections performed by STAR-48 rocket motors. The stability of this system is investigated by means of linearized equations about a uniform spin reference state. In this model, a double root does not necessarily imply instability. The resulting stability condition defines a manifold in the parameter space. A detailed study of this manifold and the parameter space shows that the envelope of the constant solutions is in fact the stability boundary. Only part of the manifold defines a physical system and the range of frequency values that make the system unstable is restricted. Also it turns out that an increase of the spring stiffness, which restrains the internal motion, does not necessarily increase the stability margin. The application of the model is demonstrated using the orbit injection data of ESA's Ulysses satellite in 1990. 相似文献
98.
99.
为了解热水火箭发动机的内弹道性能,分别在不同初始压强、不同啧喉直径、不同加水量的情况下进行了实验.获得了不同情况下发动机工作的数据.通过数据的分析,总结提出了发动机工作的四个阶段:初始段、过渡段、近似线性段和拖尾段;得出初始压强、喷喉直径、加水量对发动机内弹道性能的影响规律,同时发现了在发动机工作工程中,其压强曲线都是经历一个先急剧下降后缓慢下降的过程,但是当初始压强较低时,压强曲线在过渡段会出现一个短暂的先升后降的波动.分析得出:热水火箭发动机的比冲受初始压强值的影响较大,而与喷喉直径或者加水质量无关;常规火箭发动机的推力计算公式并不适用于热水火箭发动机. 相似文献
100.
为了研究吸气式高超声速飞行器的气动特性,提出一种新的内流阻力测量技术,即采用粒子图像测速技术和总压测量技术相结合,测量超燃发动机尾喷管流场速度矢量和皮托压力分布,间接获得内流出口处平均马赫数和内流出口处静压平均值,从而实现高超声速通气模型内流阻力测量。研究结果表明:粒子图像测速技术和总压测量技术相结合,成功地实现了内流阻力测量;试验获得的粒子图像,能够清楚地显示喷管出口位置内外流的分界面及边界层和边界层的尾迹;粒子图像测速试验获得的速度矢量场结果准确,精度高,能够提供远远超出传统测量技术所能提供的流场信息。 相似文献