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   281篇
  免费   50篇
  国内免费   73篇
航空   301篇
航天技术   51篇
综合类   31篇
航天   21篇
  2024年   1篇
  2023年   1篇
  2022年   12篇
  2021年   15篇
  2020年   19篇
  2019年   14篇
  2018年   16篇
  2017年   22篇
  2016年   26篇
  2015年   13篇
  2014年   24篇
  2013年   16篇
  2012年   22篇
  2011年   23篇
  2010年   18篇
  2009年   20篇
  2008年   18篇
  2007年   11篇
  2006年   16篇
  2005年   12篇
  2004年   4篇
  2003年   9篇
  2002年   7篇
  2001年   12篇
  2000年   2篇
  1999年   5篇
  1998年   7篇
  1997年   3篇
  1996年   2篇
  1995年   6篇
  1994年   4篇
  1993年   2篇
  1992年   4篇
  1991年   7篇
  1990年   7篇
  1989年   2篇
  1988年   1篇
  1984年   1篇
排序方式: 共有404条查询结果,搜索用时 609 毫秒
171.
双扇形孔气膜冷却效率的研究   总被引:1,自引:0,他引:1  
对平板表面的双扇形孔排气膜冷却特性进行了研究,包括孔节距、动量比和主流湍流度对气膜冷却效率的影响.气膜孔的直径为d,气膜孔与主流方向的夹角为45°.孔节距有2d,3d和4d,动量比有1,2和4,主流湍流度有0.4%和8%.结果表明,气膜冷却效率随孔节距增大而降低;孔节距为2d时,动量比增大会引起气膜冷却效率显著增加;孔节距为4d时,气膜冷却效率受动量比的影响相对较小;在孔节距及动量比均较大时,主流湍流度的增大会导致气膜冷却效率较为明显的下降.   相似文献   
172.
气膜孔形状对排孔下游换热的影响   总被引:5,自引:3,他引:2  
实验研究了气膜孔几何形状、二次流雷诺数及吹风比对孔排下游的局部换热系数的影响。所用孔形是簸箕形孔、圆锥形孔及圆柱形孔;实验的参数范围为二次流孔径雷诺数Re=10000~25000,二次流吹风比M=0.3~2.0,在上述范围选取了26个工况分别对3种孔形进行了实验。   相似文献   
173.
带60°肋U型通道中气膜孔对通道换热特性的影响   总被引:1,自引:0,他引:1  
以航空发动机涡轮叶片中段内部冷却通道为研究对象,将其简化为带肋变截面U型通道。对通道内有气膜出流时的换热特性进行了实验研究。实验模型中,矩形肋对称布置在上下2个表面,气膜孔仅布置在第2通道内。文中定义了气膜开孔率的概念,采用单元分析法研究了气膜开孔率和出流比对通道内单元努塞数分布和第2通道压力分布的影响。实验结果表明,气膜出流比一定时,随着开孔率的增加,换热增强;在两肋之间的3个气膜孔中,肋后孔对通道换热影响最大;气膜出流比与通道努塞数的关系为二次曲线。   相似文献   
174.
地球静止轨道光学遥感器的发展以及遥感器分辨率的不断提高,使得光学遥感器的口径越来越大,大口径反射镜正在成为制约遥感器性能、质量和研制成本的关键因素。本文主要围绕2m口径的超轻型反射镜开展研究,分析了定位和支撑系统的主要功能,提出了适合大口径、超轻型反射镜的定位和支撑系统方案,分析了该方案的基本原理和实现形式。  相似文献   
175.
The theoretical solutions are obtained for the three-dimensional(3-D)stress field in an infinite isotropic elastic plate with a through-the-thickness circular hole subjected to shear load at far field by using Kane and Mindlin′s assumption based on the stress function method.Based on the present solutions,the characteristics of 3-D stress field are analyzed and the emphasis is placed on the effects of the plate thickness and Poisson′s ratio on the deviation of the present 3-D in-plane stress from the related plane stress solutions,the stress concentration and the out-of-plane constraint.The present solutions show that the stress concentration factor reaches its peak value of about 8.9% which is higher than that of the plane stress solutions.As expected,the out-of-plane stress constraint factor can reach 1on the surface of the hole when the plate is a very thick one.  相似文献   
176.
本文采用动力类比法对用于核爆炸测量的空气动压探头的动态响应进行了理论分析,并对探头的三个压力量程计算了总压边和静压边进气管道中的阻尼孔直径和动压波形的上升时间。分析计算表明,在探头的三个系统中,电学系统对动态响应的影响可忽略不计;力学系统的影响也是较小的;对动态响应起主要作用的是声学系统(即管道空腔系统)。在直径为130mm 激波管中进行了全尺寸探头的动态响应实验。实验表明,阻尼孔直径和波形上升时间的实验值与计算值符合较好。此探头曾多次用于我国大气层核试验测试中。从核爆炸和激波管实验中测得的空气动压波形可看出,它们的前沿都是很好的,这反映出此探头具有良好的动态响应特性。  相似文献   
177.
We interpret the rapid correlated UV/optical/X-ray variability of XTE J1118+480 as a signature of the coupling between the X-ray corona and a jet emitting synchrotron radiation in the optical band. We propose a scenario in which the jet and the X-ray corona are fed by the same energy reservoir where large amounts of accretion power are stored before being channelled into either the jet or the high energy radiation. This time-dependent model reproduces the main features of the rapid multi-wavelength variability of XTE J1118+480. A strong requirement of the model is that the total jet power should be at least a few times larger than the observed X-ray luminosity, implying a radiative efficiency for the jet j  3 × 10−3. This would be consistent with the overall low radiative efficiency of the source. We present independent arguments showing that the jet probably dominates the energetic output of all accreting black holes in the low-hard state.  相似文献   
178.
Hard X-ray lightcurves exhibit delays of 1 s with respect to the soft X-ray lightcurves when the microquasar GRS 1915+105 is in the state of frequent, regular outbursts. Such outbursts are supposed to be driven by the radiation pressure instability of the inner disk parts. The hard X-ray delays are then caused by the time needed for the adjustment of the corona to changing conditions in the underlying disk. We support this claim by the computation of the time evolution of the disk, including a non-stationary evaporation of the disk and mass exchange with the corona.  相似文献   
179.
Coronal hole jets are fast ejections of plasma occurring within coronal holes, observed at Extreme-UltraViolet (EUV) and X-ray wavelengths. Recent observations of jets by the STEREO and Hinode missions show that they are transient phenomena which occur at much higher rates than large-scale impulsive phenomena like flares and Coronal Mass Ejections (CMEs). In this paper we describe some typical characteristics of coronal jets observed by the SECCHI instruments of STEREO spacecraft. We show an example of 3D reconstruction of the helical structure for a south pole jet, and present how the angular distribution of the jet position angles changes from the Extreme-UltraViolet-Imager (EUVI) field of view to the CORonagraph1 (COR1) (height ∼2.0 R heliocentric distance) field of view. Then we discuss a preliminary temperature determination for the jet plasma by using the filter ratio method at 171 and 195 Å and applying a technique for subtracting the EUV background radiation. The results show that jets are characterized by electron temperatures ranging between 0.8 and 1.3 MK. We present the thermal structure of the jet as temperature maps and we describe its thermal evolution.  相似文献   
180.
We present a model for neutrino flares in accreting black holes based on the injection of a non-thermal population of relativistic particles in a magnetized corona. The most important products of hadronic and photohadronic interactions at high energies are pions. Charged pions decay into muons and neutrinos; muons also decay yielding neutrinos. Taking into account these effects, coupled transport equations are solved for all species of particles and the neutrino production is estimated for the case of accreting galactic black holes.  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