全文获取类型
收费全文 | 193篇 |
免费 | 31篇 |
国内免费 | 12篇 |
专业分类
航空 | 120篇 |
航天技术 | 61篇 |
综合类 | 6篇 |
航天 | 49篇 |
出版年
2025年 | 3篇 |
2024年 | 10篇 |
2023年 | 11篇 |
2022年 | 20篇 |
2021年 | 10篇 |
2020年 | 10篇 |
2019年 | 10篇 |
2018年 | 5篇 |
2017年 | 3篇 |
2016年 | 13篇 |
2015年 | 5篇 |
2014年 | 11篇 |
2013年 | 9篇 |
2012年 | 5篇 |
2011年 | 12篇 |
2010年 | 7篇 |
2009年 | 5篇 |
2008年 | 11篇 |
2007年 | 16篇 |
2006年 | 9篇 |
2005年 | 11篇 |
2004年 | 3篇 |
2003年 | 5篇 |
2002年 | 2篇 |
2001年 | 1篇 |
2000年 | 3篇 |
1999年 | 5篇 |
1998年 | 5篇 |
1997年 | 2篇 |
1996年 | 2篇 |
1994年 | 2篇 |
1993年 | 4篇 |
1992年 | 3篇 |
1989年 | 1篇 |
1988年 | 1篇 |
1984年 | 1篇 |
排序方式: 共有236条查询结果,搜索用时 15 毫秒
51.
后加载叶型叶栅的三维压力场及其对损失发展的影响 总被引:5,自引:1,他引:5
在低速环形叶栅风洞上对具有后部加载叶型的常规直叶片叶栅和弯曲叶片叶栅进行了吹风实验,得到了两种叶栅的叶片和上、下端壁表面的静压系数分布及气动性能。实验结果表明,后部加载叶型能够建立对应优良气动特性的叶栅内部三维压力场,同时采用弯叶片技术可进一步优化展向静压系数分布。 相似文献
52.
Chen Dong Yuming Fu Guanghui Liu Hong Liu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
Minimizing energy consumption and maximizing crop productivity are major challenges to growing plants in Bioregenerative Life Support System (BLSS) for future long-term space mission. As a primary source of energy, light is one of the most important environmental factors for plant growth. The purpose of this study is to investigate the effects of low light intensity at different stages on growth, pigment composition, photosynthetic efficiency, biological production and antioxidant defence systems of wheat (Triticum aestivum L.) cultivars during ontogenesis. Experiments were divided into 3 intensity-controlled stages according to growth period (a total of 65 days): seedling stage (first 20 days), heading and flowering stage (middle 30 days) and grain filling stage (last 15 days). Initial light condition of the control was 420 μmol m−2 s−1 and the light intensity increased with the growth of wheat plants. The light intensities of group I and II at the first stage and the last stage were adjusted to the half level of the control respectively. For group III, the first and the last stage were both adjusted to half level of the control. During the middle 30 days, all treatments were kept the same intensity. The results indicated that low-light treatment at seedling stage, biomass, nutritional contents, components of inedible biomass and healthy index (including peroxidase (POD) activity, malondialdehyde (MDA) and proline content) of wheat plants have no significant difference to the control. Furthermore, unit kilojoule yield of group I reached 0.591 × 10−3 g/kJ and induced the highest energy efficiency. However, low-light treatment at grain filling stage affected the final production significantly. 相似文献
53.
54.
AP/HMX HTPB推进剂的能量特性 总被引:5,自引:1,他引:5
介绍了AP/HMX HTPB推进剂能量特性。理论计算表明,HMX取代部分AP可增加比冲,降低火焰温度和燃气中HCL含量,HMX代替20%AP,比冲增加25.46N.s.kg^-1。用BSFΩ 相似文献
55.
磁层顶磁场重联是太阳风向磁层输入能量的主要方式.重联如何触发一直是空间物理研究的难点,其机制仍然有待深入研究.由于卫星穿越磁层顶时,很难恰好穿越重联发生的区域,因此难以观测到重联的触发条件.本文利用THEMIS卫星观测,确立了反演磁层顶重联点的方法.当重联刚开始发生时,卫星能够观测到离子的能量色散特征,可利用其计算卫星到重联发生位置的距离.沿着磁力线模型追踪该距离即可反演出磁层顶发生重联的位置.与其他方法进行了对比分析,结果显示本文方法比其他方法具有更高的精度. 相似文献
56.
By use of the global PPMLR Magnetohydrodynamics (MHD) model, a serial of quasisteady- state numerical simulations were conducted to examine the modulation property of the interplanetary magnetic field clock angle θ on the solar wind energy input into the magnetosphere. All the simulations can be divided into seven groups according to different criteria of solar wind conditions. For each group, 37 numerical examples are analyzed, with the clock angle varying from 0° to 360° with an interval of 10°, keeping the other solar wind parameters (such as the solar wind number density, velocity, and the magnetic field magnitude) unchanged. As expected, the solar wind energy input into the magnetosphere is modulated by the IMF clock angle. The axisymmetrical bell-shaped curve peaks at the clock angle of 180°. However, the modulation effect remains invariant with varying other solar wind conditions. The function form of such an invariant modulation is found to be sin(θ/2)2.70 + 0.25. 相似文献
57.
J.K. Shi M.N.S. Qureshi S.Z. Ma L.D. Xia J.S. Wang 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2007,40(12):1842-1851
Considering the KuaFu mission, state of the energy release of substorm and storm is simply presented and it’s improvements by KuaFu mission are investigated. The KuaFu mission will provide us an opportunity to improve our understanding of the energy release during the storm and the substorms. The two KuaFu-B satellites flying in 180° phase-lagged formation in a polar orbit will allow synoptic observations of the auroral oval, central plasma sheet, ring current and other regions. It can monitor the polar region 24/7 continuously. The advantage of the KuaFu mission is to provide the data during all phases of storm and substorm time that can be used to study the global energy release during all phases continuously. The data from auroral imager and other in-situ instruments on board KuaFu-B can be used to study the auroral dynamics and Joule heating during a storm and substorm. The data from the neutral atom imager instrument can be used to study the dynamics and the energy release in the ring current region from sudden commencement to complete storm recovery. Furthermore the data from KuaFu-A, which is around L1 point, can be used to study the interplanetary conditions along with the data from the plasma sheet to study the triggering process and energy release during a substorm. So, KuaFu mission with its continuous time monitoring facilities would enable us to make much progress towards solving the underlying problems. 相似文献
58.
在一个异常强水平风速和极端大风切变层内, 垂直速度扰动谱表明几个相当重要特征:(1)垂直速度扰动谱有二个区域, 一个在低频区, 有谱斜率一1.65, 这个谱斜率接近于惯性子区内-5/3谱斜率, 另一个在高频区, 有谱斜率-7.11, 它接近于粘性子区内-7谱斜率.(2)垂直速度扰动谱有一个崩溃点, 约位于70m, 这与计算的内尺度有好的一致.(3)由垂直速度扰动谱计算的湍流能量耗散率是0.087m2·s-3, 这比MAP/WINE试验中得到的值约大一个数量级. 相似文献
59.
对任务星施加持续的控制加速度,使其在飞行过程中相对于目标卫星的空间位置保持不变,即实现任意位置悬停飞行。通过对任务星与目标星的相对运行分析和重力差异补偿分析,给出了在飞行过程中任务星相对于运行在椭圆轨道上的目标星实现任意位置悬停所需的径向、切向和法向控制加速度公式。最后对典型悬停飞行过程进行了动力学仿真,并对不同悬停飞行任务的能量消耗进行了对比分析,表明在一段时间内对任务星进行轨道悬停是可行的。 相似文献
60.
针对航天器进入末端能量管理段接口处时位置和航迹偏角存在大范围摄动的问题,提出一种使用迭代校正法的轨道快速生成算法。该算法可以根据航天器的具体初始状态,自动选择直接进场或者间接进场策略,快速生成可行的参考轨迹。首先通过跟踪轨迹地面投影实现侧向制导;根据末端能量管理段的起始点与终点的高度与速度约束生成参考动压-高度剖面,并跟踪此剖面实现纵向制导。然后采用迭代校正计算快速确定航向校准柱的位置与最终半径两个参数用以调整航程,保证航天器在末端的所有状态满足自动着陆段接口的边界约束。仿真结果校验了该算法可以根据航天器的具体状态快速生成符合约束条件的末端能量管理段飞行轨道,具有很好的鲁棒控制性能。 相似文献