全文获取类型
收费全文 | 2158篇 |
免费 | 471篇 |
国内免费 | 357篇 |
专业分类
航空 | 1645篇 |
航天技术 | 484篇 |
综合类 | 307篇 |
航天 | 550篇 |
出版年
2024年 | 10篇 |
2023年 | 61篇 |
2022年 | 84篇 |
2021年 | 95篇 |
2020年 | 89篇 |
2019年 | 81篇 |
2018年 | 77篇 |
2017年 | 69篇 |
2016年 | 102篇 |
2015年 | 106篇 |
2014年 | 144篇 |
2013年 | 90篇 |
2012年 | 155篇 |
2011年 | 144篇 |
2010年 | 119篇 |
2009年 | 101篇 |
2008年 | 131篇 |
2007年 | 128篇 |
2006年 | 136篇 |
2005年 | 129篇 |
2004年 | 102篇 |
2003年 | 110篇 |
2002年 | 92篇 |
2001年 | 80篇 |
2000年 | 62篇 |
1999年 | 61篇 |
1998年 | 72篇 |
1997年 | 55篇 |
1996年 | 41篇 |
1995年 | 43篇 |
1994年 | 56篇 |
1993年 | 31篇 |
1992年 | 23篇 |
1991年 | 29篇 |
1990年 | 24篇 |
1989年 | 26篇 |
1988年 | 17篇 |
1987年 | 9篇 |
1985年 | 1篇 |
1984年 | 1篇 |
排序方式: 共有2986条查询结果,搜索用时 343 毫秒
601.
In this study, the lock-in phenomenon of Tip Clearance Flow(TCF) instabilities and their relationship to blade vibration are investigated numerically on an axial transonic rotor with a large tip clearance. The capabilities of simulating instability flow and lock-in phenomenon are verified on a transonic rotor and a NACA0012 airfoil by comparing with the test data, respectively.The lock-in phenomenon is first numerically confirmed that may occur to TCF instabilities when its frequency is close to... 相似文献
602.
603.
《中国航空学报》2016,(2):448-461
In a probe and drogue aerial refueling system, the bow wave of the receiver aircraft will produce a strong aerodynamic effect on the drogue once the receiver follows the drogue at a close distance. It is a major difficulty of docking control in the probe and drogue refueling. This paper analyses the bow wave effect and presents a simple method to model it. Firstly, the inviscid flow around the receiver is modeled based on the stream function defined by basic stream singularities.Secondly, a correction function is developed to eliminate the error caused by the absence of air viscosity. Then, the aerodynamic coefficients are used to calculate the induced aerodynamic force on the drogue. The obtained model is in an analytical form that can be easily applied to the controller design and the real-time simulations. In the verification part, computational fluid dynamics(CFD)simulation tests are conducted to validate the obtained flow fields and aerodynamic forces. Finally,the modeling method is applied to an F-16 receiver aircraft in a previously developed autonomous aerial refueling simulation system. The simulations results are analyzed and compared with the NASA flight-test data, which demonstrates the effectiveness of the proposed method. 相似文献
604.
通过为数控精密磨床装配雷尼绍测头,详细介绍了在线测量在数字控精密磨床系统的构成、工作原理、数据处理方法以及磨削实验结果,使其具备在线测量功能,实现了产品的测量、加工一体化。 相似文献
605.
606.
607.
Numerical simulation of aerodynamic interaction for a tilt rotor aircraft in helicopter mode 总被引:1,自引:1,他引:0
A rotor CFD solver is developed for simulating the aerodynamic interaction phenomenon among rotor, wing and fuselage of a tilt rotor aircraft in its helicopter mode. The unsteady Navier–Stokes equations are discretized in inertial frame and embedded grid system is adopted for describing the relative motion among blades and nacelle/wing/fuselage. A combination of multi-layer embedded grid and ‘‘extended hole fringe" technique is complemented in original grid system to tackle grid assembly difficulties arising from the narrow space among different aerodynamic components, and to improve the interpolation precision by decreasing the cell volume discrepancy among different grid blocks. An overall donor cell searching and automatic hole cutting technique is used for grid assembly, and the solution processes are speeded up by introduction of Open MP parallel method. Based on this solver, flow fields and aerodynamics of a tilt rotor aircraft in hover are simulated with several rotor collective angles, and the corresponding states of an isolated rotor and rotor/wing/fuselage model are also computed to obtain reference solution.Aerodynamic interference influences among the rotor and wing/fuselage/nacelle are analyzed,and some meaningful conclusions are drawn. 相似文献
608.
为航天运载器控制系统飞行试验外、遥测数据信息管理及数据处理而研制的一个大型智能化的计算机软件,为运载器飞行试验的结果分析及制导精度的鉴定工作提供了保障条件。 相似文献
609.
610.
白刚玉对微烟推进剂燃烧性能的影响 总被引:3,自引:0,他引:3
微烟推进剂不能含有铝粉,故必须加入其他燃烧稳定剂来抑制不稳定燃烧。本文提出了燃烧稳定剂选择的关键性指标——粒度及粒度分布的可控性,认为磨料微粉白刚玉(Al_2O_3)是微烟推进剂比较合适的燃烧稳定剂新品种,进而研究了白刚玉粒度、含量对推进剂燃速、压强指数和燃烧稳定性影响的规律性,探讨了燃烧前后白刚玉粒度变化的趋势,并由实测火焰结构证实,该推进剂与双基推进剂火焰结构相似,从而为该类推进剂选择催化剂提供了理论依据. 相似文献