全文获取类型
收费全文 | 5790篇 |
免费 | 649篇 |
国内免费 | 484篇 |
专业分类
航空 | 3107篇 |
航天技术 | 1452篇 |
综合类 | 435篇 |
航天 | 1929篇 |
出版年
2024年 | 15篇 |
2023年 | 47篇 |
2022年 | 108篇 |
2021年 | 165篇 |
2020年 | 129篇 |
2019年 | 112篇 |
2018年 | 282篇 |
2017年 | 263篇 |
2016年 | 190篇 |
2015年 | 183篇 |
2014年 | 246篇 |
2013年 | 233篇 |
2012年 | 269篇 |
2011年 | 389篇 |
2010年 | 406篇 |
2009年 | 448篇 |
2008年 | 389篇 |
2007年 | 349篇 |
2006年 | 196篇 |
2005年 | 235篇 |
2004年 | 157篇 |
2003年 | 182篇 |
2002年 | 196篇 |
2001年 | 188篇 |
2000年 | 137篇 |
1999年 | 140篇 |
1998年 | 109篇 |
1997年 | 111篇 |
1996年 | 112篇 |
1995年 | 108篇 |
1994年 | 86篇 |
1993年 | 60篇 |
1992年 | 75篇 |
1991年 | 43篇 |
1990年 | 38篇 |
1989年 | 51篇 |
1988年 | 31篇 |
1987年 | 26篇 |
1986年 | 30篇 |
1985年 | 77篇 |
1984年 | 41篇 |
1983年 | 27篇 |
1982年 | 40篇 |
1981年 | 76篇 |
1980年 | 18篇 |
1978年 | 10篇 |
1977年 | 14篇 |
1976年 | 11篇 |
1975年 | 14篇 |
1974年 | 17篇 |
排序方式: 共有6923条查询结果,搜索用时 203 毫秒
341.
342.
表面热流的可辨识性分析可用于飞行器防热层内温度测量精度和测温点位置的确定,在工程上有较强的实用意义。从无量纲分析和仿真辨识出发,根据防热层材料热物性系数、测点位置、表面热流的频域特性等参数对表面热流辨识结果的影响规律,总结出了表面热流辨识问题的相似参数:基于表面热流频率参数的傅立叶数。此后,以这一傅立叶数为判据,针对不同测量误差值的情况初步建立起了表面热流可辨识性的准则和分析方法。 相似文献
343.
Yu. V. Klochkov A. P. Nikolaev A. A. Shubovich S. S. Marchenko 《Russian Aeronautics (Iz VUZ)》2013,56(4):327-334
In this paper, we present an algorithm for geometrically nonlinear finite element analysis of the shells of revolution. Use is made of the most proper algorithms for vector interpolation of displacements through the nodal unknowns and an efficient algorithm for obtaining the stress-strain increment relation at a step of loading. By comparing the results of analyzing a geometrically nonlinear shell of revolution obtained on the basis of the ANSYS software with the scalar interpolation of displacements with those obtained on the basis of an author-developed finite element, it has been shown that application of the FEM vector displacement interpolation leads to increasing the accuracy of the finite element solutions in analyzing the stress-strain state of the geometrically nonlinear shells. 相似文献
344.
345.
346.
Alexeev Igor I. Belenkaya Elena S. Bobrovnikov Sergey Yu. Kalegaev Vladimir V. 《Space Science Reviews》2003,107(1-2):7-26
A magnetohydrodynamic model of the solar wind flow is constructed using a kinematic approach. It is shown that a phenomenological
conductivity of the solar wind plasma plays a key role in the forming of the interplanetary magnetic field (IMF) component
normal to the ecliptic plane. This component is mostly important for the magnetospheric dynamics which is controlled by the
solar wind electric field. A simple analytical solution for the problem of the solar wind flow past the magnetosphere is presented.
In this approach the magnetopause and the Earth's bow shock are approximated by the paraboloids of revolution. Superposition
of the effects of the bulk solar wind plasma motion and the magnetic field diffusion results in an incomplete screening of
the IMF by the magnetopause. It is shown that the normal to the magnetopause component of the solar wind magnetic field and
the tangential component of the electric field penetrated into the magnetosphere are determined by the quarter square of the
magnetic Reynolds number. In final, a dynamic model of the magnetospheric magnetic field is constructed. This model can describe
the magnetosphere in the course of the severe magnetic storm. The conditions under which the magnetospheric magnetic flux
structure is unstable and can drive the magnetospheric substorm are discussed. The model calculations are compared with the
observational data for September 24–26, 1998 magnetic storm (Dst
min=−205 nT) and substorm occurred at 02:30 UT on January 10, 1997.
This revised version was published online in August 2006 with corrections to the Cover Date. 相似文献
347.
Frey H.U. Mende S.B. Immel T.J. Gérard J.-C. Hubert B. Habraken S. Spann J. Gladstone G.R. Bisikalo D.V. Shematovich V.I. 《Space Science Reviews》2003,109(1-4):255-283
Direct imaging of the magnetosphere by instruments on the IMAGE spacecraft is supplemented by simultaneous observations of the global aurora in three far ultraviolet (FUV) wavelength bands. The purpose of the multi-wavelength imaging is to study the global auroral particle and energy input from the magnetosphere into the atmosphere. This paper describes the method for quantitative interpretation of FUV measurements. The Wide-Band Imaging Camera (WIC) provides broad band ultraviolet images of the aurora with maximum spatial resolution by imaging the nitrogen lines and bands between 140 and 180 nm wavelength. The Spectrographic Imager (SI), a dual wavelength monochromatic instrument, images both Doppler-shifted Lyman-α emissions produced by precipitating protons, in the SI-12 channel and OI 135.6 nm emissions in the SI-13 channel. From the SI-12 Doppler shifted Lyman-α images it is possible to obtain the precipitating proton flux provided assumptions are made regarding the mean energy of the protons. Knowledge of the proton (flux and energy) component allows the calculation of the contribution produced by protons in the WIC and SI-13 instruments. Comparison of the corrected WIC and SI-13 signals provides a measure of the electron mean energy, which can then be used to determine the electron energy flux. To accomplish this, reliable emission modeling and instrument calibrations are required. In-flight calibration using early-type stars was used to validate the pre-flight laboratory calibrations and determine long-term trends in sensitivity. In general, very reasonable agreement is found between in-situ measurements and remote quantitative determinations. 相似文献
348.
349.
350.
本文利用动量矩定理推导出抽水蓄能电站水泵轮机导叶漏水量与漏水转矩的计算公式。同时在考虑漏水转矩的情况下,完成了两座抽水蓄能电站混流式水泵机组泵工况起动过渡过程的校核计算,分析了导叶间隙、漏水量等对起动过程的重要影响,过大的导叶间隙将使机组不能起动。计算分析表明,本文提出的考虑导叶间隙漏水影响进行泵工况起动过渡过程的计算方法是正确的。正确考虑漏水转矩影响,对水泵水轮机的运行特性和过滤过程的准确计算具 相似文献