全文获取类型
收费全文 | 6159篇 |
免费 | 27篇 |
国内免费 | 22篇 |
专业分类
航空 | 2875篇 |
航天技术 | 2197篇 |
综合类 | 14篇 |
航天 | 1122篇 |
出版年
2021年 | 46篇 |
2018年 | 100篇 |
2017年 | 83篇 |
2016年 | 79篇 |
2015年 | 40篇 |
2014年 | 113篇 |
2013年 | 172篇 |
2012年 | 147篇 |
2011年 | 228篇 |
2010年 | 167篇 |
2009年 | 242篇 |
2008年 | 303篇 |
2007年 | 178篇 |
2006年 | 133篇 |
2005年 | 182篇 |
2004年 | 172篇 |
2003年 | 192篇 |
2002年 | 133篇 |
2001年 | 208篇 |
2000年 | 110篇 |
1999年 | 139篇 |
1998年 | 164篇 |
1997年 | 122篇 |
1996年 | 146篇 |
1995年 | 189篇 |
1994年 | 211篇 |
1993年 | 100篇 |
1992年 | 127篇 |
1991年 | 59篇 |
1990年 | 67篇 |
1989年 | 128篇 |
1988年 | 51篇 |
1987年 | 48篇 |
1986年 | 65篇 |
1985年 | 187篇 |
1984年 | 173篇 |
1983年 | 135篇 |
1982年 | 130篇 |
1981年 | 215篇 |
1980年 | 45篇 |
1979年 | 52篇 |
1978年 | 57篇 |
1977年 | 51篇 |
1976年 | 40篇 |
1975年 | 60篇 |
1974年 | 49篇 |
1973年 | 47篇 |
1972年 | 57篇 |
1971年 | 37篇 |
1969年 | 37篇 |
排序方式: 共有6208条查询结果,搜索用时 0 毫秒
171.
Magnetospheric Multiscale Overview and Science Objectives 总被引:1,自引:0,他引:1
172.
173.
174.
For an interception strategy of a removable target by a return space vehicle (RSV), we propose a structure of the control law by the aerodynamic efficiency that determines a chain of the three standard trajectories: nosing-up–free flight–nosing-down. A solution of the terminal problem is to determine numerical values of the control parameters that define moments to switch the RSV flight from one standard trajectory to another. 相似文献
175.
Concept of monitoring for thermostressed state and service life of aircraft gas turbine engine blades 总被引:1,自引:0,他引:1
G. G. Kulikov V. A. Trushin A. I. Abdulnagimov A. A. Ganeev 《Russian Aeronautics (Iz VUZ)》2016,59(1):77-83
A concept of monitoring for material properties with residual life estimation of rotor blades for gas turbine engines is proposed. The structure of on-board control and conditionmonitoring system based on the intelligent pyrometer module with the algorithm for calculating the residual life of turbine rotor blades is described. 相似文献
176.
To calculate the unsteady helicopter motion, we propose a simplifying approach consisting in the fact that the numerical solution of equations of nonlinear nonstationary aerodynamics and flight dynamics are made successively in time intervals. As an example, the results of calculating the helicopter motion in descent are presented. The mathematical model and algorithm can be used for calculating the unsteady motion of different helicopters. 相似文献
177.
The Magnetic Field of Mercury 总被引:1,自引:0,他引:1
Brian J. Anderson Mario H. Acuña Haje Korth James A. Slavin Hideharu Uno Catherine L. Johnson Michael E. Purucker Sean C. Solomon Jim M. Raines Thomas H. Zurbuchen George Gloeckler Ralph L. McNutt Jr. 《Space Science Reviews》2010,152(1-4):307-339
The magnetic field strength of Mercury at the planet’s surface is approximately 1% that of Earth’s surface field. This comparatively low field strength presents a number of challenges, both theoretically to understand how it is generated and observationally to distinguish the internal field from that due to the solar wind interaction. Conversely, the small field also means that Mercury offers an important opportunity to advance our understanding both of planetary magnetic field generation and magnetosphere-solar wind interactions. The observations from the Mariner 10 magnetometer in 1974 and 1975, and the MESSENGER Magnetometer and plasma instruments during the probe’s first two flybys of Mercury on 14 January and 6 October 2008, provide the basis for our current knowledge of the internal field. The external field arising from the interaction of the magnetosphere with the solar wind is more prominent near Mercury than for any other magnetized planet in the Solar System, and particular attention is therefore paid to indications in the observations of deficiencies in our understanding of the external field. The second MESSENGER flyby occurred over the opposite hemisphere from the other flybys, and these newest data constrain the tilt of the planetary moment from the planet’s spin axis to be less than 5°. Considered as a dipole field, the moment is in the range 240 to 270 nT-R M 3 , where R M is Mercury’s radius. Multipole solutions for the planetary field yield a smaller dipole term, 180 to 220 nT-R M 3 , and higher-order terms that together yield an equatorial surface field from 250 to 290 nT. From the spatial distribution of the fit residuals, the equatorial data are seen to reflect a weaker northward field and a strongly radial field, neither of which can be explained by a centered-dipole matched to the field measured near the pole by Mariner 10. This disparity is a major factor controlling the higher-order terms in the multipole solutions. The residuals are not largest close to the planet, and when considered in magnetospheric coordinates the residuals indicate the presence of a cross-tail current extending to within 0.5R M altitude on the nightside. A near-tail current with a density of 0.1 μA/m2 could account for the low field intensities recorded near the equator. In addition, the MESSENGER flybys include the first plasma observations from Mercury and demonstrate that solar wind plasma is present at low altitudes, below 500 km. Although we can be confident in the dipole-only moment estimates, the data in hand remain subject to ambiguities for distinguishing internal from external contributions. The anticipated observations from orbit at Mercury, first from MESSENGER beginning in March 2011 and later from the dual-spacecraft BepiColombo mission, will be essential to elucidate the higher-order structure in the magnetic field of Mercury that will reveal the telltale signatures of the physics responsible for its generation. 相似文献
178.
Direct measurements of the geomagnetic field have been made for more than 400 years, beginning with individual determinations of the angle between geographic and magnetic North. This was followed by the start of continuous time series of full vector measurements at geomagnetic observatories and the beginning of geomagnetic repeat stations surveys in the 19th century. In the second half of the 20th century, true global coverage with geomagnetic field measurements was accomplished by magnetometer payloads on low-Earth-orbiting satellites. This article describes the procedures and instruments for magnetic field measurements on ground and in space and covers geomagnetic observatories, repeat stations, automatic observatories, satellites and historic observations. Special emphasis is laid on the global network of geomagnetic observatories. 相似文献
179.
180.
A conventional (nonmonopulse) secondary surveillance radar (SSR) is significantly cheaper than a monopulse SSR but exhibits much greater azimuthal error, especially when some of the replies are missing. Estimation techniques and their performance are discussed with special reference to SSR applications, and a novel estimator for conventional SSR is described. The proposed technique is a close approximation of the maximum-likelihood estimator (MLE), taking into account the receiver characteristics as well as the missed replies. Estimator performance obtained by analysis and computer simulation is compared with that of conventional estimators that are based on the leading and trailing edges of binary sequences and shows significantly improved accuracy 相似文献