全文获取类型
收费全文 | 5382篇 |
免费 | 814篇 |
国内免费 | 884篇 |
专业分类
航空 | 4104篇 |
航天技术 | 992篇 |
综合类 | 778篇 |
航天 | 1206篇 |
出版年
2024年 | 16篇 |
2023年 | 83篇 |
2022年 | 138篇 |
2021年 | 170篇 |
2020年 | 184篇 |
2019年 | 195篇 |
2018年 | 209篇 |
2017年 | 197篇 |
2016年 | 244篇 |
2015年 | 215篇 |
2014年 | 354篇 |
2013年 | 284篇 |
2012年 | 345篇 |
2011年 | 396篇 |
2010年 | 254篇 |
2009年 | 297篇 |
2008年 | 352篇 |
2007年 | 377篇 |
2006年 | 369篇 |
2005年 | 290篇 |
2004年 | 263篇 |
2003年 | 241篇 |
2002年 | 213篇 |
2001年 | 188篇 |
2000年 | 159篇 |
1999年 | 122篇 |
1998年 | 121篇 |
1997年 | 99篇 |
1996年 | 91篇 |
1995年 | 81篇 |
1994年 | 86篇 |
1993年 | 81篇 |
1992年 | 92篇 |
1991年 | 86篇 |
1990年 | 76篇 |
1989年 | 61篇 |
1988年 | 31篇 |
1987年 | 7篇 |
1986年 | 1篇 |
1985年 | 2篇 |
1984年 | 10篇 |
排序方式: 共有7080条查询结果,搜索用时 140 毫秒
951.
952.
Extensive experimental studies on the heat transfer characteristics of two rows of aligned jet holes impinging on a concave surface in a wing leading edge were conducted, where50000 Rej 90000, 1.74 H/d 27.5, 66° a 90°, and 13.2 r/d 42.03. The finding was that the heat transfer performance at the jet-impingement stagnation point with two rows of aligned jet holes was the same as that with a single row of jet holes or the middle row of three-row configurations when the circumferential angle of the two jet holes was larger than 30°. The attenuation coefficient distribution of the jet impingement heat transfer in the chordwise direction was so complicated that two zones were divided for a better analysis. It indicated that: the attenuation coefficient curve in the jet impingement zone exhibited an approximate upside-down bell shape with double peaks and a single valley; the attenuation coefficient curve in the non-jet impingement zone was like a half-bell shape, which was similar to that with three rows of aligned jet holes; the factors,including Rej, H/d and r/d, affected the attenuation coefficient value at the valley significantly.When r/d was increased from 30.75 to 42.03, the attenuation rates of attenuation coefficient increased only by 1.8%. Consequently, experimental data-based correlation equations of the Nusselt number for the heat transfer at the jet-impingement stagnation point and the distributionof the attenuation coefficient in the chordwise direction were acquired, which play an important role in designing the wing leading edge anti-icing system with two rows of aligned jet holes. 相似文献
953.
Aya Bamba Hiroya Yamaguchi Katsuji Koyama Junko S. Hiraga Steve Holt John P. Hughes Hideaki Katagiri Jun Kataoka Satoru Katsuda Shunji Kitamoto Motohide Kokubun Hironori Matsumoto Emi Miyata Koji Mori Hiroshi Nakajima Masanobu Ozaki Rob Petre Akiko Sekiguchi Tadayuki Takahashi Takaaki Tanaka Yukikatsu Terada Hiroshi Tomida Yohko Tsuboi Masahiro Tsujimoto Hiroshi Tsunemi Yasunobu Uchiyama Masaru Ueno Shin Watanabe 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(3):411-415
SN 1006 is one of the supernova remnants (SNRs) with relatively low-temperature electrons, considering the young age of just 1000 years. We carried out SN 1006 mapping observations with the X-ray Imaging Spectrometers (XIS) and the Hard X-ray Detector (HXD) onboard Suzaku, the fifth Japanese X-ray satellite. Thanks to the excellent spectral resolution of XIS in the soft X-ray band, H-like and He-like oxygen emission lines were clearly detected, and we could make a map of the line intensity, and as well as a flux and the photon index of nonthermal component. We found that these parameters have spatial dependences from region to region in the SNR; the north region is bright in nonthermal, while dim in thermal; the east region is bright in both nonthermal and thermal; the inner region shows dim nonthermal and bright thermal emission. The photon index is the smallest in the north region. 相似文献
954.
根据**飞机上,CW-1002和Ⅱ-5的试飞结果,对两种产品的性能做了对比分析;对飞行中大气温度的获取方法提出了的新意见。 相似文献
955.
Yihua Zheng Anthony T.Y. Lui Mei-Ching Fok Brian J. Anderson Pontus C. Brandt Donald G. Mitchell 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(8):1234-1242
One essential component of magnetosphere and ionosphere coupling is the closure of the ring current through Region 2 field-aligned current (FAC). Using the Comprehensive Ring Current Model (CRCM), which includes magnetosphere and ionosphere coupling by solving the kinetic equation of ring current particles and the closure of the electric currents between the two regions, we have investigated the effects of high latitude potential, ionospheric conductivity, plasma sheet density and different magnetic field models on the development of Region 2 field-aligned currents, and the relationship between R2 FACs and the ring current. It is shown that an increase in high latitude potential, ionospheric conductivity or plasma sheet density generally results in an increase in Region 2 FACs’ intensity, but R2 FACs display different local time and latitudinal distributions for changes in each parameter due to the different mechanisms involved. Our simulation results show that the magnetic field configuration of the inner magnetosphere is also an important factor in the development of Region 2 field-aligned current. More numerical experiments and observational results are needed in further our understanding of the complex relationship of the two current systems. 相似文献
956.
通过大量的事实,阐述了在企业不断深化改革过程中,开创社会化计量测试的基础,条件及基本做法。 相似文献
957.
没有农业的现代化就没有中国农业生产现代化,通过分析我国农业现代化的基本现状和存在的问题,提出了只有提高农业劳动生产率,开拓现代农业新领域,调整产业结构,发挥比较优势,坚持科教兴农,走集约化农业发展道路,我国农业的现代化和社会主义新农村建设才能取得更大的成效。 相似文献
958.
冯根尧 《郑州航空工业管理学院学报(管理科学版)》2008,26(3):57-59
中小企业群是目前国际上产业规划的流行模式。我国中小企业群具有生产运用战略纵向一体化,原材料供应方式灵活多变,经营方式专业化以及制造技术相对落后等特征。建立供需链管理模式下的地方网络体系,实施大规模定制的生产运作模式,一方面可以提高中小企业自身的管理与运作水平,还能把不同的具有产业关联的中小企业联结成一个整体,形成资源合力,加速中小企业发展,提升中小企业群的核心竞争力。 相似文献
959.
基本公共服务均等化研究现状与展望 总被引:1,自引:0,他引:1
基本公共服务均等化概念一经提出,迅速成为学术界研究的热点之一。学者主要从宏观社会政策、社会公正、公共财政等视角对基本公共服务均等化的内涵、供给问题、供给内容与途径等方面进行了研究。完善社会政策、注重社会公正、合理重构公共财政体制是公共服务均等化的必要途径。目前基本公共服务供给协调机制尤其是激励机制的研究亟待加强,基本公共服务均等化与大部制改革研究有待推进和深化。 相似文献
960.
飞机稳定尾旋的预测研究 总被引:3,自引:0,他引:3
在考虑各种影响因素的基础上,增加了交叉惯性积对稳定尾旋的影响,从而导出了分析稳定尾旋的有关公式。为了避免遗漏解的可能性,采用不需选择初值的求解方法,给出了稳定尾旋的判据。应用该方法对某型飞机的尾旋进行了预测计算,求出了一个陡尾旋解和一个平尾旋解,计算结果与该飞机尾旋试飞结果吻合较好,表明计算方法是正确的,计算结果可用于指导飞机的尾旋试飞。 相似文献