全文获取类型
收费全文 | 909篇 |
免费 | 125篇 |
国内免费 | 226篇 |
专业分类
航空 | 583篇 |
航天技术 | 328篇 |
综合类 | 128篇 |
航天 | 221篇 |
出版年
2024年 | 3篇 |
2023年 | 20篇 |
2022年 | 26篇 |
2021年 | 31篇 |
2020年 | 31篇 |
2019年 | 39篇 |
2018年 | 42篇 |
2017年 | 33篇 |
2016年 | 52篇 |
2015年 | 34篇 |
2014年 | 58篇 |
2013年 | 57篇 |
2012年 | 69篇 |
2011年 | 73篇 |
2010年 | 50篇 |
2009年 | 77篇 |
2008年 | 68篇 |
2007年 | 63篇 |
2006年 | 71篇 |
2005年 | 44篇 |
2004年 | 29篇 |
2003年 | 36篇 |
2002年 | 35篇 |
2001年 | 28篇 |
2000年 | 25篇 |
1999年 | 23篇 |
1998年 | 21篇 |
1997年 | 22篇 |
1996年 | 10篇 |
1995年 | 19篇 |
1994年 | 24篇 |
1993年 | 13篇 |
1992年 | 8篇 |
1991年 | 13篇 |
1990年 | 5篇 |
1989年 | 4篇 |
1988年 | 3篇 |
1984年 | 1篇 |
排序方式: 共有1260条查询结果,搜索用时 421 毫秒
781.
《中国航空学报》2016,(2):386-394
Vortex/flame interaction is an important mechanism for unsteady combustion in a swirl combustion system. Technology of low emission stirred swirl(Te LESS), which is characterized with stratified swirl flow, has been developed in Beihang University to reduce NOXemission. However,large-scale flow structure would be induced in strong swirl flow. Experiments and computational fluid dynamics(CFD) simulation were carried out to investigate the unsteady flow feature and its mechanism in Te LESS combustor. Hotwire was firstly applied to testing the unsteady flow feature and a distinct mode with 2244 Hz oscillation frequency occurred at the pilot swirl outlet.The flow mode amplitude decayed convectively. Large eddy simulation(LES) was then applied to predicting this flow mode and know about its mechanism. The deviation of mode prediction compared with hotwire test was 0.8%. The spiral isobaric structure in pilot flow passage indicates that precessing vortex core(PVC) existed. The velocity spectrum and phase lag analysis suggest that the periodic movement at the pilot outlet was dominated by precessing movement. Negative tangential momentum gradient reflects that the swirl flow was unstable. Another phenomenon was found out that the PVC movement was intermittently rotated along the symmetric axis. 相似文献
782.
783.
Traditional Global Sensitivity Analysis (GSA) focuses on ranking inputs according to their contributions to the output uncertainty.However,information about how the specific regions inside an input affect the output is beyond the traditional GSA techniques.To fully address this issue,in this work,two regional moment-independent importance measures,Regional Importance Measure based on Probability Density Function (RIMPDF) and Regional Importance Measure based on Cumula tive Distribution Function (RIMCDF),are introduced to find out the contributions of specific regions of an input to the whole output distribution.The two regional importance measures prove to be reasonable supplements of the traditional GSA techniques.The ideas of RIMPDF and RIMCDF are applied in two engineering examples to demonstrate that the regional moment-independent importance analysis can add more information concerning the contributions of model inputs. 相似文献
784.
为了借鉴美国加强基础研究工作的经验,促进我国基础研究的发展,研究了近年来美国国会、国防部及一些研究机构关于基础研究的咨询报告和评估报告。总结了美国加强基础研究的主要措施,包括:加大政府投入力度、减少行政部门干预、加强与大学合作、建设政府科研机构、发挥项目经理作用和制定明确的科技战略等。并针对我国基础研究工作的不足,提出了加强基础研究的投入力度、稳定从事基础研究的科技队伍、改进基础研究的项目管理等建议。 相似文献
785.
786.
Panagiota Petkaki Alexander L. MacKinnon 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
Release of stored magnetic energy via particle acceleration is a characteristic feature of astrophysical plasmas. Magnetic reconnection is one of the mechanisms for releasing energy from magnetized plasmas. Collisionless magnetic reconnection could provide both the energy release mechanism and the particle accelerator in space plasmas. Here we studied particle acceleration when fluctuating (in-time) electric fields are superposed on an static X-type magnetic field in collisionless hot solar plasma. This system is chosen to mimic the reconnective dissipation of a linear MHD disturbance. Our results are compared to particle acceleration from constant electric field superposed on an X-type magnetic field. The constant electric field configuration represents the effects of steady state magnetic reconnection. Time evolution of ion and electron distributions are obtained by numerically integrating particle trajectories. The frequencies of the electric field represent a turbulent range of waves. Depending on the frequency and amplitude of the electric field, electrons and ions are accelerated to different degrees and have energy distributions of bimodal form consisting of a lower energy part and a high energy tail. For frequencies (ω in dimensioless units) in the range 0.5 ? ω ? 1.0 a substantial fraction (20%–30%) of the proton distribution is accelerated to gamma-ray producing energies. For frequencies in the range 1 ? ω ? 100.0 the bulk of the electron distribution is accelerated to hard X-ray producing energies. The acceleration mechanism is important for solar flares and solar noise storms but it could be applicable to all collisionless astrophysical plasmas. 相似文献
787.
788.
789.
790.
大载荷摆动情况下飞行器姿态控制研究(英文) 总被引:2,自引:0,他引:2
天文观测卫星的主敏感器安装在一个具有二自由度、并直接与卫星平台相连的万向支架上。因敏感器的质量和长度不能忽略,故卫星姿态及其质心位置、转动惯量等结构参数将因敏感器与卫星间的角运动而发生改变,因此大载荷摆动情况下的飞行器姿态控制是本文研究的重点。本文根据动量矩定理推导出了存在内部相对运动的二刚体动力学模型,卫星系统的转动惯量将由该模型确定。由卫星的当前及其期望姿态四元数,构建出描述卫星姿态偏差的拟欧拉角;对拟欧拉角进行规范化处理,以保证三通道所对应的拟欧拉角分量分别由控制力矩的3个分量所控制。之后,提出了基于拟欧拉角的姿态开关控制律,该控制律可保证三通道所对应的相轨迹可沿开关线滑向坐标原点(其期望状态)。仿真结果表明,即使是在结构不对称和三通道严重耦合的情况下,该控制律也能保证卫星姿态可以得到较好的控制。 相似文献