首页 | 本学科首页   官方微博 | 高级检索  
文章检索
  按 检索   检索词:      
出版年份:   被引次数:   他引次数: 提示:输入*表示无穷大
  收费全文   241篇
  免费   76篇
  国内免费   23篇
航空   198篇
航天技术   62篇
综合类   37篇
航天   43篇
  2023年   10篇
  2022年   13篇
  2021年   13篇
  2020年   17篇
  2019年   14篇
  2018年   19篇
  2017年   11篇
  2016年   18篇
  2015年   18篇
  2014年   21篇
  2013年   14篇
  2012年   12篇
  2011年   16篇
  2010年   15篇
  2009年   5篇
  2008年   21篇
  2007年   7篇
  2006年   10篇
  2004年   2篇
  2003年   8篇
  2002年   3篇
  2001年   4篇
  2000年   4篇
  1999年   3篇
  1998年   12篇
  1997年   10篇
  1996年   10篇
  1995年   5篇
  1994年   1篇
  1993年   9篇
  1992年   1篇
  1990年   3篇
  1989年   2篇
  1987年   1篇
  1986年   2篇
  1985年   1篇
  1983年   2篇
  1982年   1篇
  1980年   1篇
  1969年   1篇
排序方式: 共有340条查询结果,搜索用时 31 毫秒
51.
以垂直/短距起降飞机过渡飞行状态为背景,针对机翼内埋式风扇布局的自由来流/风扇喷流混合型流动,基于结构/非结构混合网格使用CFD方法进行了非定常数值模拟和分析.首先使用滑移网格技术对NASA涵道螺旋桨进行算例验证,其时均计算结果与实验值的误差为5.3%,证明了计算方法的可靠性和准确性,然后数值模拟了机翼内埋式风扇布局在不同迎角下的气动性能.结果表明:风扇喷流在机翼上产生了特有的“抽吸”和“堵塞”效应,引起了机翼总升阻力的显著增加,升力最大增量达到干净机翼升力的2.6倍,阻力最大增量为干净机翼阻力的3.2倍,混合流场在机翼后缘引起了升力损失并卷起对涡.   相似文献   
52.
基于拟动力学的航空发动机主轴球轴承热弹流润滑分析   总被引:3,自引:2,他引:1  
以航空发动机主轴球轴承高速高温重载典型工况为算例,基于轴承拟动力学分析,得到滚动体与套圈之间的微接触区运动和受力状态,分别用Hamrock-Dowson(H-D)拟合公式和翟文杰热修正公式计算了最小膜厚(MFT),同时结合热弹流润滑分析得到最小膜厚分布,对比了试验测试、H-D拟合、翟文杰热修正和热弹流润滑分析4种算法的最小膜厚,并根据膜厚比判定了轴承的弹流润滑状态.结果表明:H-D拟合和翟文杰热修正最小膜厚与试验测试结果相差较远,热弹流润滑分析结果与试验数据吻合性较好,误差10%以内;探讨了不同工况下的轴承弹流润滑性能.结果表明:存在径向载荷时,润滑膜整体压力增大,膜厚减小;随着转速增大,压力减小,膜厚增大,但是增大的趋势减缓.   相似文献   
53.
The problem of target motion analysis (TMA) has been the subject of an important literature. However, present methods use data estimated by a short time analysis (azimuths, Dopplers, etc.). For far sources, the nonstationarities of the array processing outputs, induced by the sources motion, may be simply modeled. This model leads one to consider directly a spatio-temporal TMA. Then new (spatio-temporal) data can be estimated. These estimates correspond to a long time analysis. Further, note that they are estimated independently of the (classical) bearings. In this general framework, the concept of source trajectory replaces the classical instantaneous bearings. Corresponding TMA algorithms are then studied. Then the study of statistical performance is carefully studied  相似文献   
54.
超声速射流逆流通常用于导弹、航天飞机、卫星和飞船等飞行器运动状态的控制。欠膨胀超声速射流逆流的流场包含有多激波(如弓形激波和马赫盘)、接触间断和剪切层,其结构非常复杂。本文采用激波高分辨率有限差分(TVD)格式,对恒定自由流条件,各种不同射流出出口压比的超声速轴对称逆射流进行了数值模拟,且对各种条件下的物理现象给予了分析。计算的马赫盘和弓形激波位置与实验值相吻合,为此类流动问题提供了一种有效的预测  相似文献   
55.
首次提出了一种固有模态函数积检测器。首先通过经验模式分解(EMD)把带噪信号分解成有限个固有模态函数(IMF)。检测的基本思路是,对各个IMF分量的绝对值作逐点乘积,用于抑制噪声并凸现信号,最后进行滤波和判决。本文以UWB信号为例,数据源于UWB雷达实验系统。在低信噪比(SNR),UWB脉冲与噪声波形相似,且噪声概率密度函数(PDF)未知情况下,进行实验。结果表明,当峰峰信噪比低于5dB时,该检测器性能优于Teager能量算子(TEO)。  相似文献   
56.
Recently much attention has been focused on the transient behavior of the magnetopause in response to pressure pulses and southward fluctuations of the interplanetary magnetic field. We examine the motion of the magnetopause behind the foreshock and conclude that this motion is affected by foreshock pressure variations but not by fluctuations in the direction of the magnetic field. Neither magnetopause erosion nor flux transfer event occurrence is controlled by the foreshock. On the contrary, flux transfer events occur at times of steady IMF and thier quasi-periodic behavior is controlled by the magnetopause or the magnetosphere and is not driven by the external boundary conditions. Since flux transfer events are clearly due to reconnection, this observation implies that the IMF must be southward some time perhaps as long as 7 minutes before flux transfer begins.  相似文献   
57.
The effects of gravity waves on OH and 5577 0I emissions have been used to investigate (1) the possible production of “secondary” waves or “ripples” by a “primary” wave; (2) the possible application of such observed optical emissions for computing atmospheric parameters such as turbulence viscosity in the mesospheric regions.  相似文献   
58.
The performance analysis of source trajectory estimation using measurements provided by multiple platforms (or arrays) is studied. In numerous practical situations, the maneuvering ability of the receiver (e.g., a ship towing linear arrays) is limited, leading to the assumption that the observer motion is rectilinear and uniform. Even if this hypothesis appears quite restrictive, practical and tactical considerations fully justify its interest. This leads to consider multiple (platform) target motion analysis (denoted MTMA) and to analyze the performance of such trajectory estimation methods  相似文献   
59.
The delivery of extraterrestrial organic materials to primitive Earth from meteorites or micrometeorites has long been postulated to be one of the origins of the prebiotic molecules involved in the subsequent apparition of life. Here, we report on experiments in which vacuum UV photo-irradiation of interstellar/circumstellar ice analogues containing H(2)O, CH(3)OH, and NH(3) led to the production of several molecules of prebiotic interest. These were recovered at room temperature in the semi-refractory, water-soluble residues after evaporation of the ice. In particular, we detected small quantities of hydantoin (2,4-imidazolidinedione), a species suspected to play an important role in the formation of poly- and oligopeptides. In addition, hydantoin is known to form under extraterrestrial, abiotic conditions, since it has been detected, along with various other derivatives, in the soluble part of organic matter of primitive carbonaceous meteorites. This result, together with other related experiments reported recently, points to the potential importance of the photochemistry of interstellar "dirty" ices in the formation of organics in Solar System materials. Such molecules could then have been delivered to the surface of primitive Earth, as well as other telluric (exo-) planets, to help trigger first prebiotic reactions with the capacity to lead to some form of primitive biomolecular activity.  相似文献   
60.
首次提出了一种固有模态函数积检测器.首先通过经验模式分解(EMD)把带噪信号分解成有限个固有模态函数(IMF).检测的基本思路是,对各个IMF分量的绝对值作逐点乘积,用于抑制噪声并凸现信号,最后进行滤波和判决.本文以UWB信号为例,数据源于UWB雷达实验系统.在低信噪比(SNR),UWB脉冲与噪声波形相似,且噪声概率密度函数(PDF)未知情况下,进行实验.结果表明,当峰峰信噪比低于5 dB时,该检测器性能优于Teager能量算子(TEO).  相似文献   
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号