全文获取类型
收费全文 | 2610篇 |
免费 | 15篇 |
国内免费 | 12篇 |
专业分类
航空 | 1229篇 |
航天技术 | 887篇 |
综合类 | 13篇 |
航天 | 508篇 |
出版年
2021年 | 25篇 |
2019年 | 15篇 |
2018年 | 41篇 |
2017年 | 26篇 |
2016年 | 27篇 |
2014年 | 55篇 |
2013年 | 72篇 |
2012年 | 54篇 |
2011年 | 122篇 |
2010年 | 76篇 |
2009年 | 120篇 |
2008年 | 114篇 |
2007年 | 68篇 |
2006年 | 60篇 |
2005年 | 67篇 |
2004年 | 76篇 |
2003年 | 87篇 |
2002年 | 46篇 |
2001年 | 62篇 |
2000年 | 53篇 |
1999年 | 55篇 |
1998年 | 75篇 |
1997年 | 47篇 |
1996年 | 75篇 |
1995年 | 83篇 |
1994年 | 59篇 |
1993年 | 51篇 |
1992年 | 65篇 |
1991年 | 33篇 |
1990年 | 20篇 |
1989年 | 53篇 |
1988年 | 28篇 |
1987年 | 24篇 |
1986年 | 31篇 |
1985年 | 101篇 |
1984年 | 55篇 |
1983年 | 56篇 |
1982年 | 61篇 |
1981年 | 76篇 |
1980年 | 25篇 |
1979年 | 29篇 |
1978年 | 28篇 |
1977年 | 26篇 |
1976年 | 20篇 |
1975年 | 21篇 |
1974年 | 22篇 |
1973年 | 15篇 |
1970年 | 20篇 |
1969年 | 19篇 |
1967年 | 17篇 |
排序方式: 共有2637条查询结果,搜索用时 0 毫秒
831.
A major source of transonic and supersonic wind-tunnel test data uncertainty are angle-of-attack-measurement errors caused by unknown sting and balance deflections under load. Since dynamic loads in pressurized or cryogenic wind tunnels generally exceed those in conventional low-speed atmospheric wind tunnels, the need to account for these distortions during model testing is even more acute. A novel laser-based instrument for the in-situ measurement of wind-tunnel-model angle of attack that enables continuous, time-dependent measurements to be made without signal dropout is described. Proof-of-concept experiments, along with the results of recent measurements conducted at the NASA Ames 9-ft×7-ft supersonic wind tunnel, are presented. Experiments were also conducted to determine the reliable range, sensitivity, and long-term stability of the instrument. The results show that 0.01° sensitivity can be achieved and that optical and detector packaging requirements are less stringent than those for current tilt-sensor or accelerometer model installations 相似文献
832.
C. T. Russell J. G. Luhmann F. R. Fenrich 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2001,28(12):1707-1716
The Polar satellite has explored the high-latitude, high-latitude magnetosphere out to 9 Earth radii (Re). The magnetic field data returned from this mission can be used both to provide data for new empirical models and to test existing models. Tests include comparing the observed location of the polar cusp with its position in the empirical models and comparing the strength of the magnetic field in the surrounding region. Near the cusp the magnetosphere is quite sensitive to solar wind conditions. In particular the energy density of the cusp plasma depends on the pressure of the solar wind applied to the interface of the cusp and the sheath. The applied pressure in turn depends on the shape of the magnetopause and the orientation of that interface, both controlled by the direction of the interplanetary magnetic field. Magnetohydrodynamic (MHD) models provide a coarse picture of the magnetosphere at high latitudes. While generally quite realistic, these too require testing against observations because even the MHD models must make some simplifying assumptions. 相似文献
833.
The US Air Force future vision for information fusion is presented in the context of results of a study of long-term challenges in the science and technology of command and control and the programs of the Air Force designed to meet them. A new approach to research is presented that takes advantage of scientific challenge problems that are operationally validated in collaboration with research laboratories in government and industry. 相似文献
834.
O'Neill M.J. McDanal A.J. Piszczor M.F. George P.J. Edwards D.L. Brandhorst H.W. Eskenazi M.I. Botke M.M. Jaster P.M. 《Aerospace and Electronic Systems Magazine, IEEE》2003,18(1):3-9
At IECEC 2001, this team presented a paper on the new stretched lens array (SLA), including its evolution from the successful SCARLET array on the NASA/JPL Deep Space 1 spacecraft. Since that conference, the SLA team has made significant advances in SLA technology, including component-level improvements, array-level optimization, space environment exposure testing, and prototype hardware fabrication and evaluation. This paper describes the evolved version of the SLA, highlighting recent improvements in the lens, solar cell, photovoltaic receiver, rigid panel structure, and complete solar array wing. In addition to excellent durability in the space environment, the near-term SLA will provide outstanding wing-level performance parameters: 180 W/kg specific power; 300 W/m/sup 2/ power density; 300 V operational voltage; 85% savings in cell area (cm/sup 2//W) and cell-related cost ($/W) compared to planar arrays; 9 kW/m/sup 3/ stowed power at launch. 相似文献
835.
Slaveski F. Sluss J. Jr. Atiquzzaman M. Nguyen H. Ngo D. 《Aerospace and Electronic Systems Magazine, IEEE》2003,18(8):3-8
During flight, aircraft avionics transmit and receive RF signals to/from antennas over coaxial cables. As the density and complexity of onboard avionics increases, the electromagnetic interference (EMI) environment degrades proportionately, leading to decreasing signal-to-noise ratios (SNRs) and potential safety concerns. The coaxial cables are inherently lossy, limiting the RF signal bandwidth while adding considerable weight. To overcome these limitations, we have investigated a fiber optic communications link for aircraft that utilizes wavelength division multiplexing (WDM) to support the simultaneous transmission of multiple signals (including RF) over a single optical fiber. Optical fiber has many advantages over coaxial cable, particularly lower loss, greater bandwidth, and immunity to EMI. In this paper, we demonstrate that WDM can be successfully used to transmit multiple RF signals over a single optical fiber with no appreciable signal degradation. We investigate the transmission of FM and AM analog modulated signals, as well as FSK digital modulated signals, over a fiber optic link (FOL) employing WDM. We present measurements of power loss, delay, SNR, carrier-to-noise ratio (CNR), total harmonic distortion (THD), and bit error rate (BER). Our experimental results indicate that WDM is a fiber optic technology suitable for avionics applications. 相似文献
836.
M Nelson J Allen A Alling W F Dempster S Silverstone 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2003,31(7):1649-1655
The parallels between the challenges facing bioregenerative life support in artificial closed ecological systems and those in our global biosphere are striking. At the scale of the current global technosphere and expanding human population, it is increasingly obvious that the biosphere can no longer safely buffer and absorb technogenic and anthropogenic pollutants. The loss of biodiversity, reliance on non-renewable natural resources, and conversion of once wild ecosystems for human use with attendant desertification/soil erosion, has led to a shift of consciousness and the widespread call for sustainability of human activities. For researchers working on bioregenerative life support in closed systems, the small volumes and faster cycling times than in the Earth's biosphere make it starkly clear that systems must be designed to ensure renewal of water and atmosphere, nutrient recycling, production of healthy food, and safe environmental methods of maintaining technical systems. The development of technical systems that can be fully integrated and supportive of living systems is a harbinger of new perspectives as well as technologies in the global environment. In addition, closed system bioregenerative life support offers opportunities for public education and consciousness changing of how to live with our global biosphere. 相似文献
837.
Dempsey P.J. Handschuh R.F. Afjeh A.A. 《Aerospace and Electronic Systems Magazine, IEEE》2003,18(9):11-17
A diagnostic tool for detecting damage to spiral bevel gears was developed. Two different monitoring technologies - oil debris analysis and vibration were integrated using data fusion into a health monitoring system for detecting surface fatigue pitting damage on gears. This integrated system showed improved detection and decision-making capabilities as compared to using individual monitoring technologies. This diagnostic tool was evaluated by collecting vibration and oil debris data from fatigue tests performed in the NASA Glenn Spiral Bevel Gear Fatigue Rigs. Data was collected during experiments performed in this test rig when pitting damage occurred. Results show that combining the vibration and oil debris measurement technologies improves the detection of pitting damage on spiral bevel gears. 相似文献
838.
Cooperation is a major theme of international space law but the law and history also recognize the existence of competition and conflict. What are the trend lines in terms of promoting collective goods, commercialization and new military uses of space? An overview of selected major laws and policies, as they relate to cooperation, competition and conflict, combined with a theoretical examination of game theory (zero-sum and non-zero sum games), will enable us to obtain an overall understanding of the space age and the choices that space lawyers and policy makers face in the future. 相似文献
839.
The problems are considered of a modelling research of navigation features and improvement of the navigating filters algorithms used in the navigating devices of ground mobile vehicles (MV). It is supposed that the methods and approaches known as real time kinematic (RTK) are incorporated in a basis of researched navigating devices and algorithms. Thus, the measurements from satellite navigating systems such as GLONASS/GPS, and also the measurements from other traditional measuring means (tactile sensors, steering wheel angle and/or inertial measuring instruments) are used in the navigating device of the MV. In the present report we solve the problems and describe the methods of a modeling research of the features of functional units algorithms of the MV navigating processor with account of a satellite navigation set integration with other measuring instruments. The improvement of these devices interaction is made by means of the computer complex "AutoMobil," allowing us to simulate the certain conditions of these navigating tools operation. The imitation computer complex "AutoMobil" for researches of the MV navigation is developed within the frameworks of a programming environment "Delphi-7". 相似文献
840.
Sidhwa F. Moore F. Williams T. Matsuura D. 《Aerospace and Electronic Systems Magazine, IEEE》2004,19(7):31-36
In today's world of constrained budgets, one of the problems the military faces is the challenge of trying to maintain organic maintenance capabilities. Historically, the US Air Force has desired to achieve an autonomous capability to maintain the equipment it uses. This has been achieved, traditionally, by setting-up three levels of maintenance: organizational; intermediate (back-shop); and depot. The I-level back-shops often utilize militarized automatic test equipment (ATE) and test program sets (TPSs) to test today's complex aircraft line replaceable units (LRUs). And even though this is still a cost-effective maintenance philosophy, it has become costly to develop militarized ATE. The Department of Defense (DoD) has been very active in trying to reduce the total ownership cost of ATE in the government inventory. One approach is to utilize commercial, instead of Mil-Spec, ATE. However, utilizing commercial ATE at an USAF back-shop is not without its tradeoffs and challenges as it represents a significant deviation from the way the USAF maintenance squadrons are accustomed to "doing business." This paper documents the current success story of replacing the legacy C-17 I-level ATE with a commercial ATE. 相似文献