全文获取类型
收费全文 | 584篇 |
免费 | 157篇 |
国内免费 | 114篇 |
专业分类
航空 | 436篇 |
航天技术 | 141篇 |
综合类 | 105篇 |
航天 | 173篇 |
出版年
2024年 | 2篇 |
2023年 | 14篇 |
2022年 | 33篇 |
2021年 | 37篇 |
2020年 | 42篇 |
2019年 | 27篇 |
2018年 | 38篇 |
2017年 | 26篇 |
2016年 | 29篇 |
2015年 | 33篇 |
2014年 | 40篇 |
2013年 | 41篇 |
2012年 | 36篇 |
2011年 | 43篇 |
2010年 | 49篇 |
2009年 | 38篇 |
2008年 | 29篇 |
2007年 | 40篇 |
2006年 | 32篇 |
2005年 | 27篇 |
2004年 | 13篇 |
2003年 | 16篇 |
2002年 | 18篇 |
2001年 | 12篇 |
2000年 | 18篇 |
1999年 | 17篇 |
1998年 | 13篇 |
1997年 | 16篇 |
1996年 | 9篇 |
1995年 | 8篇 |
1994年 | 8篇 |
1993年 | 13篇 |
1992年 | 9篇 |
1991年 | 7篇 |
1990年 | 5篇 |
1989年 | 3篇 |
1988年 | 3篇 |
1987年 | 4篇 |
1986年 | 2篇 |
1985年 | 2篇 |
1982年 | 1篇 |
1981年 | 1篇 |
1965年 | 1篇 |
排序方式: 共有855条查询结果,搜索用时 190 毫秒
501.
飞行器在大气中飞行,不可避免地受到阵风的影响。阵风所附加的气动载荷引发飞行器飞行状态的改变,过大幅值的阵风影响飞行的性能与安全。针对这种状况,首先采用改进的Lamb-Ossen涡模型,建立尾涡形式的阵风场;然后采用基于CFD技术的非定常N-S方程求解,并在计算网格中引入"网格速度"来模拟阵风,对SWIM(Subsonic Wall Interference Model)尾涡中的定常气动特性进行验证;最后通过CFD-6DOF的耦合,对SWIM俯冲穿越尾涡场的飞行轨迹进行研究。结果表明:计算结果与实验值符合较好;SWIM在尾涡中飞行时出现抖动、下沉、改变飞行状态、剧烈翻转的现象,与实际飞行器进入尾涡中的轨迹特性类似。 相似文献
502.
斜激波与弓形激波相互作用形成的波系结构可以分为六类,其中IV型激波干扰产生了超声速"喷流",产生了极高的热载和压载。基于彩虹纹影显示技术,实验获得了六类激波干扰彩虹纹影照片,分析了各类激波干扰的波系结构。通过数值计算,获得了有无斜激波干扰的条件下,壁面附近温度与压强的分布,讨论了IV型激波干扰产生极高热载和压载的原因。研究表明,激波干扰发生以后,钝头体表明压载与热载急剧增加,尤其是IV型激波干扰,形成的超声速"喷流"射向钝头体壁面的超声速射流,会导致峰值压力剧烈升高,其数量相当于来流静压的近40倍,驻点附近的热流升高将近8倍。 相似文献
503.
High-order compact finite volume methods on unstructured grids with adaptive mesh refinement for solving inviscid and viscous flows 总被引:1,自引:0,他引:1
In the present paper, high-order finite volume schemes on unstructured grids developed in our previous papers are extended to solve three-dimensional inviscid and viscous flows. The high-order variational reconstruction technique in terms of compact stencil is improved to reduce local condition numbers. To further improve the efficiency of computation, the adaptive mesh refinement technique is implemented in the framework of high-order finite volume methods. Mesh refinement and coarsening criteria are chosen to be the indicators for certain flow structures. One important challenge of the adaptive mesh refinement technique on unstructured grids is the dynamic load balancing in parallel computation. To solve this problem, the open-source library p4est based on the forest of octrees is adopted. Several two- and three-dimensional test cases are computed to verify the accuracy and robustness of the proposed numerical schemes. 相似文献
504.
Neutral density shows complicated temporal and spatial variations driven by external forcing of the thermosphere/ionosphere system, internal dynamics, and thermosphere and ionosphere coupling. Temporal variations include abrupt changes with a time scale of minutes to hours, diurnal variation, multi-day variation, solar-rotational variation, annual/semiannual variation, solar-cycle variation, and long-term trends with a time scale of decades. Spatial variations include latitudinal and longitudinal variations, as well as variation with altitude. Atmospheric drag on satellites varies strongly as a function of thermospheric mass density. Errors in estimating density cause orbit prediction error, and impact satellite operations including accurate catalog maintenance, collision avoidance for manned and unmanned space flight, and re-entry prediction. In this paper, we summarize and discuss these density variations, their magnitudes, and their forcing mechanisms, using neutral density data sets and modeling results. The neutral density data sets include neutral density observed by the accelerometers onboard the Challenging Mini-satellite Payload (CHAMP), neutral density at satellite perigees, and global-mean neutral density derived from thousands of orbiting objects. Modeling results are from the National Center for Atmospheric Research (NCAR) thermosphere-ionosphere-electrodynamics general circulation model (TIE-GCM), and from the NRLMSISE-00 empirical model. 相似文献
505.
506.
Fuzzy norm method for evaluating random vibration of airborne platform from limited PSD data 总被引:1,自引:1,他引:1
For random vibration of airborne platform, the accurate evaluation is a key indicator to ensure normal operation of airborne equipment in flight. However, only limited power spectral density(PSD) data can be obtained at the stage of flight test. Thus, those conventional evaluation methods cannot be employed when the distribution characteristics and priori information are unknown. In this paper, the fuzzy norm method(FNM) is proposed which combines the advantages of fuzzy theory and norm theory. The proposed method can deeply dig system information from limited data, which probability distribution is not taken into account. Firstly, the FNM is employed to evaluate variable interval and expanded uncertainty from limited PSD data, and the performance of FNM is demonstrated by confidence level, reliability and computing accuracy of expanded uncertainty. In addition, the optimal fuzzy parameters are discussed to meet the requirements of aviation standards and metrological practice. Finally, computer simulation is used to prove the adaptability of FNM. Compared with statistical methods, FNM has superiority for evaluating expanded uncertainty from limited data. The results show that the reliability of calculation and evaluation is superior to 95%. 相似文献
507.
采用通快TruDisk 4002光纤激光器在TC4合金表面分别制备了0wt% Y2O3和3wt% Y2O3的TC4+Ni45+Co-WC钛基耐磨复合涂层。利用XRD、SEM、EDS、EPMA、显微硬度计和摩擦磨损试验机等分析了涂层组织、显微硬度和摩擦学性能。结果表明,两种涂层表面均无裂纹孔隙等缺陷,且生成相一致,主要包括TiC、TiB2、Ti2Ni、WC和α-Ti;0wt% Y2O3涂层组织存在明显偏析,析出相尺寸粗大且方向性明显;3wt% Y2O3涂层组织呈均匀弥散状态分布,细化特征明显;经Bramfitt二维点阵错配度计算,(100)Y2O3和(100)Ti2Ni、(111)Y2O3和(110)TiC、(110)Y2O3和(1010)TiB2间的错配度分别为5.75%、6.72%和10.10%,Y2O3作为异质形核核心对Ti2Ni、TiC和TiB2的细化能力依次为Ti2Ni > TiC > TiB2;0wt% Y2O3和3wt% Y2O3涂层显微硬度分别为600~630 HV0.5和470~480 HV0.5,较基材分别提高了约62%和26%;3wt% Y2O3涂层耐磨减摩性最优,其磨损体积和摩擦系数较0wt% Y2O3涂层分别下降了约47.8%和5.0%,磨损机制主要为磨粒磨损。 相似文献
508.
509.
The effects of laser shock peening (LSP) on improving fatigue life of aluminum alloy 7050 are investigated.Surface hardness is increased corresponding to a high dislocation density induced by LSP.The X-ray diffraction stress measurement shows that LSP results in prominent increase of surface compressive stress,quasi-symmetrically distributed in the laser peened region.The fatigue life of the alloy 7050 in rivet fastener hole structure is notably improved owing to LSP.The sequence of LSP and fastener hole preparation also influence the fatigue cycle life of the alloy. 相似文献
510.
血药浓度在位检测仪的光路设计 总被引:1,自引:1,他引:0
介绍了血药浓度在位检测仪的光路设计,重点阐述发如何降低光能的损耗。该仪器利用Y型光纤束把紫外光照射到血液中的药物上,再把药物发出的荧光收集并送到检测器,其信号供计算机实时采集。 相似文献