全文获取类型
收费全文 | 2211篇 |
免费 | 384篇 |
国内免费 | 447篇 |
专业分类
航空 | 1407篇 |
航天技术 | 654篇 |
综合类 | 383篇 |
航天 | 598篇 |
出版年
2024年 | 5篇 |
2023年 | 29篇 |
2022年 | 45篇 |
2021年 | 63篇 |
2020年 | 76篇 |
2019年 | 47篇 |
2018年 | 59篇 |
2017年 | 65篇 |
2016年 | 75篇 |
2015年 | 96篇 |
2014年 | 121篇 |
2013年 | 124篇 |
2012年 | 120篇 |
2011年 | 145篇 |
2010年 | 166篇 |
2009年 | 173篇 |
2008年 | 149篇 |
2007年 | 121篇 |
2006年 | 110篇 |
2005年 | 98篇 |
2004年 | 62篇 |
2003年 | 66篇 |
2002年 | 64篇 |
2001年 | 81篇 |
2000年 | 95篇 |
1999年 | 110篇 |
1998年 | 115篇 |
1997年 | 104篇 |
1996年 | 87篇 |
1995年 | 57篇 |
1994年 | 61篇 |
1993年 | 45篇 |
1992年 | 43篇 |
1991年 | 46篇 |
1990年 | 29篇 |
1989年 | 24篇 |
1988年 | 25篇 |
1987年 | 16篇 |
1986年 | 10篇 |
1985年 | 4篇 |
1984年 | 3篇 |
1983年 | 1篇 |
1982年 | 2篇 |
1981年 | 2篇 |
1979年 | 2篇 |
1965年 | 1篇 |
排序方式: 共有3042条查询结果,搜索用时 31 毫秒
981.
近年来,我国民用航空事业持续健康发展,一方面是现有的各大机场航班量不断创造新高,另一方面是支线民用航空机场的不断涌现。进入二十一世纪我国的民航事业又迎来了一个蓬勃发展的大好时机,2004年我国的航空运输总周转量已跃居世界第三。在民航总局的领导下,民航业勇于面对机遇 相似文献
982.
从简单的数学模型出发,利用直观的温度及浓度分布假设,对生物体冻结过程中的传热、传质进行了理论分析,并将结果与精确解及测量值进行了比较。其解法简单,省去了以往的有限差分求解的繁琐的计算过程,并且计算结果与试验数据吻合得很好。 相似文献
983.
人—机—环境系统设计中人的性能研究 总被引:2,自引:0,他引:2
为了提高人-机-环境系统的性能特性,目前发展了以人为核心的人-机-环境系统设计思想,本文结合该设计思想,进一步分析了人-机-环境系统中人的性能研究的主要方面,提出了多因素耦合作用下人机特性模型将成为今后的主要研究方向。 相似文献
985.
Michael Juntao Yuan Beverley J. Wills 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2004,34(12):2599-2603
Changes in Eddington accretion ratios are thought to result in X-ray spectral index changes in Galactic binary black hole systems. Objects with higher Eddington ratios have softer X-ray spectra. Can we apply this result to much more massive black hole systems such as QSOs? If so, X-ray observations will give us valuable insight into the physics of QSOs. Among QSOs, X-ray spectral index is part of a large set of correlated optical and UV observational properties, especially optical Fe II and [O III] strengths in the Hβ region. To investigate whether this set of correlations is related to Eddington ratio, we use as probes, BALQSOs that have been suggested to be youthful super-accretors. We conducted infrared spectroscopy of the Hβ rest wavelength region for a sample of BALQSOs and compared line measurements with those for high and low redshift non-BAL QSOs. Hβ line widths and bolometric luminosity are used to calculate QSO black hole masses and Eddington ratios. Our results support the hypothesis that optical Fe II and [O III] line strengths are Eddington ratio indicators in QSO central engines. A possible explanation is that strong Fe II and weak [O III] indicate abundant cold gas that could fuel near Eddington accretion. 相似文献
986.
987.
988.
An improved method to determine cutting force coefficients for bull-nose cutters is proposed based on the semi-mechanistic cutting force model. Due to variations of cutting speed along the tool axis in bull-nose milling, they affect coefficients significantly and may bring remarkable discrepancies in the prediction of cutting forces. Firstly, the bull-nose cutter is regarded as a finite number of axial discs piled up along the tool axis, and the rigid cutting force model is exerted. Then through discretization along cutting edges, the cutting force related to each element is recalculated, which equals to differential force value between the current and previous elements. In addition, coefficient identification adopts the cubic polynomial fitting method with the slice elevation as its horizontal axis. By calculating relations of cutting speed and cutting depth, the influences of speed variations on cutting force can be derived. Thereby, several tests are conducted to calibrate the coefficients using the improved method, which are applied to later force predictions. Eventually, experimental evaluations are discussed to verify the effectiveness. Compared to the conventional method, the results are more accurate and show satisfactory consistency with the simulations. For further applications, the method is instructive to predict the cutting forces in bull-nose milling with lead or tilt angles and can be extended to the selection of cutting parameters. 相似文献
989.
This paper intends to provide theoretical basis for matching design of hydraulic load simulator (HLS) with aerocraft actuator in hardware-in-loop test, which is expected to help actuator designers overcome the obstacles in putting forward appropriate requirements of HLS. Traditional research overemphasizes the optimization of parameters and methods for HLS controllers. It lacks deliberation because experimental results and project experiences indicate different ultimate performance of a specific HLS. When the actuator paired with this HLS is replaced, the dynamic response and tracing precision of this HLS also change, and sometimes the whole system goes so far as to lose control. Based on the influence analysis of the preceding phenomena, a theory about matching design of aerocraft actuator with HLS is presented, together with two paired new concepts of "Standard Actuator" and "Standard HLS". Further research leads to seven important conclusions of matching design, which suggest that appropriate stiffness and output torque of HLS should be carefully designed and chosen for an actuator. Simulation results strongly support that the proposed principle of matching design can be anticipated to be one of the design criteria for HLS, and successfully used to explain experimental phenomena and project experiences. 相似文献
990.
Constructing high approximation accuracy surrogate model with lower computational cost has great engineering significance. In this paper, using co-Kriging method, an efficient multifidelity surrogate model is constructed based on two independent high and low fidelity samples. Co-Kriging method can use a greater quantity of low-fidelity information to enhance the accuracy of a surrogate of the high-fidelity model by modeling the correlation between high and low fidelity model, thus computational cost of building surrogate model can be greatly reduced. A wing-body problem is taken as an example to compare characteristics of co-Kriging multi-fidelity (CKMF) model with traditional Kriging based multi-fidelity (KMF) model. A sampling convergence of the CKMF model and the KMF model is conducted, and an appropriate sampling design is selected through the sampling convergence analysis. The results indicate that CKMF model has higher approximation accuracy with the same high-fidelity samples, and converges at less high-fidelity samples. A wing-body drag reduction optimization design using genetic algorithm is implemented. Satisfying design results are obtained, which validate the feasibility of CKMF model in engineering design. 相似文献