全文获取类型
收费全文 | 667篇 |
免费 | 152篇 |
国内免费 | 84篇 |
专业分类
航空 | 516篇 |
航天技术 | 130篇 |
综合类 | 53篇 |
航天 | 204篇 |
出版年
2023年 | 16篇 |
2022年 | 30篇 |
2021年 | 30篇 |
2020年 | 31篇 |
2019年 | 33篇 |
2018年 | 31篇 |
2017年 | 41篇 |
2016年 | 49篇 |
2015年 | 34篇 |
2014年 | 39篇 |
2013年 | 43篇 |
2012年 | 49篇 |
2011年 | 46篇 |
2010年 | 55篇 |
2009年 | 53篇 |
2008年 | 47篇 |
2007年 | 47篇 |
2006年 | 28篇 |
2005年 | 27篇 |
2004年 | 21篇 |
2003年 | 16篇 |
2002年 | 28篇 |
2001年 | 16篇 |
2000年 | 18篇 |
1999年 | 4篇 |
1998年 | 13篇 |
1997年 | 7篇 |
1996年 | 11篇 |
1995年 | 6篇 |
1994年 | 5篇 |
1993年 | 6篇 |
1992年 | 5篇 |
1991年 | 5篇 |
1990年 | 3篇 |
1989年 | 4篇 |
1988年 | 5篇 |
1987年 | 1篇 |
排序方式: 共有903条查询结果,搜索用时 375 毫秒
811.
To investigate the deflection effect of gas plasma plume controlled by magnetic field, a novel experimental scheme was presented. The Cs2CO3 catalytic ionization seeds were injected into the combustion chamber to obtain gas plasma on a high temperature magneto hydrodynamic (MHD) experiment rig. The plasma jet was deflected under the action of an external magnetic field, resulting in a thrust-vector effect. Particle image velocimetry (PIV) collected two-dimensional images of jet flow field. Through image processing and velocity vector analysis, the jet deflection angle can be obtained quantitatively. At 1800-2500K, the jet deflection was verified experimentally under the condition of 0.45T magnetic field strength. The results indicate that the jet deflection angle increases gradually with the increase of gas temperature, and above 2200K, the jet deflection angle increase obviously. In the process of gas plasma jet, it is feasible to realize the jet deflection controlled by MHD by adding an external magnetic field. 相似文献
812.
航空发动机推力衰退缓解的神经网络控制 总被引:1,自引:0,他引:1
针对航空发动机气路部件性能退化导致的推力下降问题,提出一种基于变增量线性规划(LP)优化 神经网络控制方法用于航空发动机推力衰退缓解控制。该方法通过内环控制转速和发动机压比,外环修正发动机指令信号以缓解发动机推力衰退。其中内环非线性自回归滑动平均(NARMA-L2)转速控制器由神经网络训练得到;外环指令修正回路利用变增量LP优化方法调整发动机指令信号。以某型小涵道比涡扇发动机为对象进行仿真验证,结果表明,在4组仿真条件下,设计的控制方法在保证性能退化的发动机不超限的条件下使推力衰退至少缓解了46.5%,验证了该方法的有效性。 相似文献
813.
结合国外的相关研究工作,对新型无叶栅反推力装置的气动性能进行研究和分析,利用康达效应提高新型无叶栅反推力装置的工作效率。计算结果表明,利用康达效应可以使新型反推力装置的轴向反推力系数从0.175提高到0.36。此种反推力装置与常规叶栅式反推力装置相比,质量大大减轻,适合应用在大涵道比涡扇发动机上。 相似文献
814.
815.
816.
817.
J. Büchner 《Space Science Reviews》2006,122(1-4):149-160
Current sheets are essential for energy dissipation in the solar corona, in particular by enabling magnetic reconnection.
Unfortunately, sufficiently thin current sheets cannot be resolved observationally and the theory of their formation is an
unresolved issue as well. We consider two predictors of coronal current concentrations, both based on geometrical or even
topological properties of a force-free coronal magnetic field. First, there are separatrices related to magnetic nulls. Through
separatrices the magnetic connectivity changes discontinuously. Coronal magnetic nulls are, however, very rare. Second, inspired
by the concept of generalized magnetic reconnection without nulls, quasi-separatrix layers (QSL) were suggested. Through QSL
the magnetic connectivity changes continuously, though strongly. The strength of the connectivity change can be quantified
by measuring the squashing of the flux tubes which connect the magnetically conjugated photospheres.
We verify the QSL and separatrix concepts by comparing the sites of magnetic nulls and enhanced squashing with the location
of current concentrations in the corona. Due to the known difficulties of their direct observation, we simulated coronal current
sheets by numerically calculating the response of the corona to energy input from the photosphere, heating a simultaneously
observed Extreme Ultraviolet Bright Point. We did not find coronal current sheets at separatrices but at several QSL locations.
The reason is that, although the geometrical properties of force-free extrapolated magnetic fields can indeed hint at possible
current concentrations, a necessary condition for current sheet formation is the local energy input into the corona. 相似文献
818.
Supermaneuver flight is often operated withhigh angle- of- attack and high angular rates.Su-per- maneuver flight cannot be controlled by aconventional gain- scheduled controller but canbe controlled by using a nonlinear dynamic- in-version controller[1~ 3] . This paper presents a method to use twokinds of controllers,nonlinear dynamic- inver-sion and conventional gain- scheduled con-trollers,in a flight control system.The nonlin-ear dynamic- inversion controller is used to con-trol superm… 相似文献
819.
复合材料混合模式分层断裂的实验表征 总被引:1,自引:0,他引:1
介绍了一种碳纤维增强复合材料混合模式层间断裂试验方法,它采用改进的混合模式弯曲试验构型,可对Ⅰ型对Ⅱ型断裂按比例加载,且使用对开裂的梁形试件。 相似文献
820.
为了分析推力室壁应力和变形分布情况,研究推力室失效位置和失效机理,建立了一种弹塑性有限元分析方法。建立推力室一维流动传热模型,为结构弹塑性分析提供输入。进一步建立推力室壁在温度和压强载荷下的二维弹塑性计算模型,分析了在预冷-工作-后冷-关机的工作循环下推力室壁的应力应变响应,比较了温度载荷和压强载荷的作用程度,并预估了推力室使用寿命。结果表明:推力室壁产生的弹塑性变形是由温度载荷和压强载荷共同作用所致,温度载荷起主导作用。推力室内壁冷却通道中心位置最先发生失效破坏,限制了推力室的使用寿命。从计算时间和准确性来说,该方法能够为再生冷却通道的优化设计和性能估算提供参考。 相似文献