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211.
212.
This paper presents a status of the ARIANE 5 launch vehicle dynamic environments after the 5 first flights. It concerns mainly the low frequency vibrations, the acoustic and the shocks that the payloads experience and the related external excitations. The flight measurement plan is described. The results show that the frequencies are well characterized and the levels are low pointing out margins with regard to the specifications Furthermore, one describe the efficiency of attenuation solutions implemented to reduce the payload environments. 相似文献
213.
Le Contel Olivier Perraut Sylvaine Roux Alain Pellat René 《Space Science Reviews》2001,95(1-2):415-426
For <bi,be, the electron and ion bounce frequencies, the response of a plasma to an externally applied electromagnetic perturbation is nonlocal. This implies, via the quasi-neutrality equation, the development of an electrostatic potential which is constant for a given magnetic field line. In the near equatorial region the corresponding potential electric field is shown to oppose the effect of the induced electric field associated with the externally applied perturbation. Thus the effect of the induced electric field is partially shielded; the total azimuthal electric field (i.e. induced plus potential) tends to be small, which explains why the radial flow velocity is slow during quasi-steady conditions prevailing during the growth phase and after the active phase. The nonlocal response of the plasma also leads to the development of a parallel current that may generate current driven Alfvén (CDA) waves, which mode convert into shear Alfvén (SA) waves. CDA/SA waves are systematically observed at early breakup; they grow very fast and produce a parallel diffusion of electrons. As soon as the diffusion time is shorter than the bounce time (d<b), the nonlocal response vanishes. Thus the shielding disappears, and an enhanced transport is restored at the rate fixed by the induced electric field alone. We show that fast flows effectively occur when CDA waves have enough power to diffuse electrons (over d<b). Electron parallel diffusion also leads to an interruption of the parallel current and therefore to a disruption of the perpendicular current. 相似文献
214.
再入钝头体近尾流动计算 总被引:2,自引:0,他引:2
本文采用联立求解粘性剪切层和有旋元粘区的方法计算了再入钝头体层流近尾流场,有旋无粘区采用有旋特征线法计算,粘性剪切层采用改进的流管法计算,这两个区域间的基本流线上的压力,温度,速度等由两个区域迭代匹配确定,粘性剪切层的下边界区分流线采用的实验确定,回避了回流区复杂计算,计算结果与有关试验和文献一致,本文的目的是提供远尾流计算所需的颈部初剖面。 相似文献
215.
D. A. Gurnett W. S. Kurth D. L. Kirchner G. B. Hospodarsky T. F. Averkamp P. Zarka A. Lecacheux R. Manning A. Roux P. Canu N. Cornilleau-Wehrlin P. Galopeau A. Meyer R. Boström G. Gustafsson J.-E. Wahlund L. Åhlen H. O. Rucker H. P. Ladreiter W. Macher L. J. C. Woolliscroft H. Alleyne M. L. Kaiser M. D. Desch W. M. Farrell C. C. Harvey P. Louarn P. J. Kellogg K. Goetz A. Pedersen 《Space Science Reviews》2004,114(1-4):395-463
The Cassini radio and plasma wave investigation is designed to study radio emissions, plasma waves, thermal plasma, and dust in the vicinity of Saturn. Three nearly orthogonal electric field antennas are used to detect electric fields over a frequency range from 1 Hz to 16 MHz, and three orthogonal search coil magnetic antennas are used to detect magnetic fields over a frequency range from 1 Hz to 12 kHz. A Langmuir probe is used to measure the electron density and temperature. Signals from the electric and magnetic antennas are processed by five receiver systems: a high frequency receiver that covers the frequency range from 3.5 kHz to 16 MHz, a medium frequency receiver that covers the frequency range from 24 Hz to 12 kHz, a low frequency receiver that covers the frequency range from 1 Hz to 26 Hz, a five-channel waveform receiver that covers the frequency range from 1 Hz to 2.5 kHz in two bands, 1 Hz to 26 Hz and 3 Hz to 2.5 kHz, and a wideband receiver that has two frequency bands, 60 Hz to 10.5 kHz and 800 Hz to 75 kHz. In addition, a sounder transmitter can be used to stimulate plasma resonances over a frequency range from 3.6 kHz to 115.2 kHz. Fluxes of micron-sized dust particles can be counted and approximate masses of the dust particles can be determined using the same techniques as Voyager. Compared to Voyagers 1 and 2, which are the only spacecraft that have made radio and plasma wave measurements in the vicinity of Saturn, the Cassini radio and plasma wave instrument has several new capabilities. These include (1) greatly improved sensitivity and dynamic range, (2) the ability to perform direction-finding measurements of remotely generated radio emissions and wave normal measurements of plasma waves, (3) both active and passive measurements of plasma resonances in order to give precise measurements of the local electron density, and (4) Langmuir probe measurements of the local electron density and temperature. With these new capabilities, it will be possible to perform a broad range of studies of radio emissions, wave-particle interactions, thermal plasmas and dust in the vicinity of Saturn.DeceasedThis revised version was published online in July 2005 with a corrected cover date. 相似文献
216.
217.
以CaCO3和Ca(H2PO4)2.H2O[钙磷比n(Ca)/n(P)=1.67]的混合物为前驱体,在超声波辅助下,水热法制备了纳米羟基磷灰石(n-HAP)。利用X射线衍射仪、电子透射电镜、傅里叶红外吸收光谱仪对制备的羟基磷灰石进行表征。并从前驱物溶液的配制、晶体成核、晶体生长等方面探讨了羟基磷灰石纳米晶体形成的机理。 相似文献
218.
O.?Le?ContelEmail author P.?Leroy A.?Roux C.?Coillot D.?Alison A.?Bouabdellah L.?Mirioni L.?Meslier A.?Galic M.?C.?Vassal R.?B.?Torbert J.?Needell D.?Rau I.?Dors R.?E.?Ergun J.?Westfall D.?Summers J.?Wallace W.?Magnes A.?Valavanoglou G.?Olsson M.?Chutter J.?Macri S.?Myers S.?Turco J.?Nolin D.?Bodet K.?Rowe M.?Tanguy B.?de?la?Porte 《Space Science Reviews》2016,199(1-4):257-282
The tri-axial search-coil magnetometer (SCM) belongs to the FIELDS instrumentation suite on the Magnetospheric Multiscale (MMS) mission (Torbert et al. in Space Sci. Rev. (2014), this issue). It provides the three magnetic components of the waves from 1 Hz to 6 kHz in particular in the key regions of the Earth’s magnetosphere namely the subsolar region and the magnetotail. Magnetospheric plasmas being collisionless, such a measurement is crucial as the electromagnetic waves are thought to provide a way to ensure the conversion from magnetic to thermal and kinetic energies allowing local or global reconfigurations of the Earth’s magnetic field. The analog waveforms provided by the SCM are digitized and processed inside the digital signal processor (DSP), within the Central Electronics Box (CEB), together with the electric field data provided by the spin-plane double probe (SDP) and the axial double probe (ADP). On-board calibration signal provided by DSP allows the verification of the SCM transfer function once per orbit. Magnetic waveforms and on-board spectra computed by DSP are available at different time resolution depending on the selected mode. The SCM design is described in details as well as the different steps of the ground and in-flight calibrations. 相似文献
219.
为了研究温度升高对翼型表面空化流动的影响,以水为介质,首先对几种现有空化模型的预测能力进行了对比分析,发现Singhal模型能够较准确预测空化区的形状、压力和温度分布。通过添加空化引起的能量源项、耦合介质物性参数与温度关系等方式考虑了热力学效应的影响,并利用现有实验数据充分验证了仿真方法的可靠性,发现考虑热力学效应对压力分布影响较小,但是会导致空化区最大温降减小10%左右。基于建立的仿真方法,对298K~393K温度范围内空化流动进行数值仿真,发现空化区温降随温度升高而增大,但是空化区面积随温度变化在T=353K存在拐点,T353K时,空化区面积随温度升高而增大;而T≥353K时,空化区随温度升高而减小。最后研究了雷诺数变化对空化发展的影响,发现雷诺数增大有一定促进作用,而温度升高同时导致热力学效应增强(抑制空化)和雷诺数增大(促进空化),正是这两种相反作用之间的平衡决定着温度对空化流动的影响。 相似文献
220.