全文获取类型
收费全文 | 5399篇 |
免费 | 33篇 |
国内免费 | 18篇 |
专业分类
航空 | 2334篇 |
航天技术 | 1915篇 |
综合类 | 191篇 |
航天 | 1010篇 |
出版年
2021年 | 45篇 |
2019年 | 41篇 |
2018年 | 122篇 |
2017年 | 88篇 |
2016年 | 73篇 |
2015年 | 35篇 |
2014年 | 137篇 |
2013年 | 147篇 |
2012年 | 136篇 |
2011年 | 230篇 |
2010年 | 165篇 |
2009年 | 252篇 |
2008年 | 282篇 |
2007年 | 158篇 |
2006年 | 136篇 |
2005年 | 154篇 |
2004年 | 150篇 |
2003年 | 165篇 |
2002年 | 210篇 |
2001年 | 223篇 |
2000年 | 86篇 |
1999年 | 125篇 |
1998年 | 143篇 |
1997年 | 118篇 |
1996年 | 135篇 |
1995年 | 161篇 |
1994年 | 116篇 |
1993年 | 77篇 |
1992年 | 118篇 |
1991年 | 43篇 |
1990年 | 42篇 |
1989年 | 97篇 |
1988年 | 43篇 |
1987年 | 40篇 |
1986年 | 41篇 |
1985年 | 159篇 |
1984年 | 138篇 |
1983年 | 91篇 |
1982年 | 115篇 |
1981年 | 151篇 |
1980年 | 56篇 |
1979年 | 31篇 |
1978年 | 37篇 |
1977年 | 27篇 |
1976年 | 28篇 |
1975年 | 33篇 |
1974年 | 33篇 |
1972年 | 26篇 |
1971年 | 27篇 |
1969年 | 31篇 |
排序方式: 共有5450条查询结果,搜索用时 93 毫秒
221.
N. Singh B. I. Vashi 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1992,12(12):53-56
Collection of electrons by a long conducting cylinder in a flowing plasma is studied by means of numerical simulations. The plasma flow simulates the relative motion between a spacecraft and plasma. The sheath structures and the levels of electron current collections for the cases with and without an ambient magnetic field (
) are studied. It is found that for the flow perpendicular to the magnetic field, the current is considerably enhanced depending on the relative drift velocity. In the case of a non-zero magnetic field perpendicular to the cylinder axis, the potential structure is a two-dimensional double layer with dimensions L L|, where L and L| are the dimensions perpendicular and parallel to
, respectively. L is found to be the current limiting radius given by the Parker-Murphy model. For the flow along
, the electron current is found to be smaller than that for the flow perpendicular to
. This is explained in terms of the potential structures. 相似文献
222.
A. Kiraga Z. K
os V. N. Oraevsky V. C. Dokukin S. A. Pulinets 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1995,15(12):21-24
There were several cases when modulated electron beam had been injected from APEX satellite into an otherwise unmodified ionospheric plasma. The beams were formed from 2 μs pulses repeated at a rate of 40kHz. Injections took place in the altitude range 400–1100km over Europe. The onboard receiver connected to the dipole antenna swept the frequency interval 1–10 MHz in 1 sec. Due to a relatively narrow receiver bandwidth (15 kHz), moderate frequency step (50 kHz), slow changes of fn and fc (local electron plasma and gyro frequencies) fine structure of excited emissions was detected. In many cases, a very prominent doublet could be convincingly identified as a (fn,fu=sqrt(fn*fn+fc*fc)) band, with fn practically equal to the local plasma frequency in the unperturbed ionosphere. Determination of plasma frequency is of prime importance in analysis of complex structures composed from various harmonics fn,fc,fu. Complexity is manifested as coalescing of various harmonics with maxima shifted from nominal frequencies or splitting them into components due to mixing of local and propagation effects. Despite the existence of strong emissions on frequencies characteristic for the unperturbed ionosphere, very strong broadcasting transmissions are frequently cut off, even when the beam is directed upward. Most typical spectra are discussed. 相似文献
223.
S. Mereghetti A. Tiengo P. Esposito G. Vianello A. De Luca D. Götz G. Weidenspointner A. von Kienlin G.L. Israel L. Stella N. Rea R. Turolla S. Zane 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
We describe the results obtained with Target of Opportunity observations of the galactic sources SGR 1627–41 and 1E 1547–5408. These two transients show several similarities supporting the interpretation of Anomalous X-ray Pulsars and Soft Gamma-ray Repeaters as a single class of strongly magnetized neutron stars. 相似文献
224.
P.T. Gallagher C.A. Young J.P. Byrne R.T.J. McAteer 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
Coronal mass ejections (CMEs) are large-scale eruptions of plasma and magnetic field that can produce adverse space weather at Earth and other locations in the Heliosphere. Due to the intrinsic multiscale nature of features in coronagraph images, wavelet and multiscale image processing techniques are well suited to enhancing the visibility of CMEs and suppressing noise. However, wavelets are better suited to identifying point-like features, such as noise or background stars, than to enhancing the visibility of the curved form of a typical CME front. Higher order multiscale techniques, such as ridgelets and curvelets, were therefore explored to characterise the morphology (width, curvature) and kinematics (position, velocity, acceleration) of CMEs. Curvelets in particular were found to be well suited to characterising CME properties in a self-consistent manner. Curvelets are thus likely to be of benefit to autonomous monitoring of CME properties for space weather applications. 相似文献
225.
V.E. Kunitsyn A.M. Padokhin A.E. Vasiliev G.A. Kurbatov V.L. Frolov G.P. Komrakov 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
The purpose of this work is to report the experimental evidences for the influence of perturbations in the electron density in the dayside mid-latitude ionosphere, that are caused by high-frequency heating of the F2 layer, on the GNSS signals. The experiments were carried out at the Sura heater (Radio Physical Research Institute, N. Novgorod). During the sessions of ionospheric heating with different time modulations of the radiated power the rays linking the navigational satellites with the ground receiver intersected the heated region. Variations in the total electron content (TEC) were studied; these variations are proportional to the reduced phases of navigational signals. It is shown that with the square-wave modulation of the radiated power (with periods of 1, 6, 10 and 15 min), perturbations with periods of the main modulation of heating and its harmonics appear in the spectrum of TEC variations. Examples are presented of identification of the heating-induced variations in TEC, including determination of the amplitudes and time characteristics of these variations. 相似文献
226.
227.
N. I. Akishev I. I. Zakirov V. A. Ivanov V. N. Paimushin M. A. Shishov 《Russian Aeronautics (Iz VUZ)》2011,54(2):115-124
The known analytical solutions of the linearized stability problems for rectangular hinged plates under the combined loading
are generalized to the similar problems for skew plates, the deformation mechanics of which is described by the equations
of the classical theory formed in the oblique Cartesian coordinates. 相似文献
228.
In this paper, we examine experimentally some devices the principle of action of which is based on using the dynamic pressure
of air extracted to engine cooling and which are meant for reducing the radial temperature gradient in GTE rotor disks. We
established that the devices equipped with the ejector channels make it possible to accelerate the process of the disk hub
heating by hot air suction from the cavity periphery towards the rotor axis of rotation. Using the data of visualization studies,
we show the possibility for efficient operation of ejector devices in the conditions of real GTE rotor circumferential velocities. 相似文献
229.
The basic steps of an algorithm are given for calculating the parameters of the limiting state of a helicopter main rotor
blade. To estimate the static strength, a technique of elastic constants variation is used; it is based on the limit equilibrium
theory and enables us to obtain the upper and lower bounds for the critical load simultaneously. An iterative technique is
proposed to determine the lower bound of the allowable load on the root section of the composite blade depending on the azimuthal
angle of its turn in the helicopter hovering mode. 相似文献
230.
N. M. Bodunov 《Russian Aeronautics (Iz VUZ)》2011,54(1):89-94
A mathematical model of the process of bending and rolling the thin-walled components is presented taking into account the
geometrical nonlinearity. Also presented is the technique for calculating the setup variables of bending equipment, which
is based on reduction of the initial differential boundary-value problem to the discrete one with the use of the finite difference
method. 相似文献