全文获取类型
收费全文 | 178篇 |
免费 | 10篇 |
专业分类
公路运输 | 32篇 |
综合类 | 20篇 |
水路运输 | 112篇 |
铁路运输 | 18篇 |
综合运输 | 6篇 |
出版年
2024年 | 2篇 |
2023年 | 1篇 |
2022年 | 4篇 |
2021年 | 9篇 |
2020年 | 5篇 |
2019年 | 2篇 |
2018年 | 7篇 |
2017年 | 6篇 |
2016年 | 6篇 |
2015年 | 12篇 |
2014年 | 21篇 |
2013年 | 6篇 |
2012年 | 17篇 |
2011年 | 8篇 |
2010年 | 6篇 |
2009年 | 14篇 |
2008年 | 10篇 |
2007年 | 9篇 |
2006年 | 15篇 |
2005年 | 4篇 |
2004年 | 2篇 |
2003年 | 6篇 |
2002年 | 1篇 |
2001年 | 1篇 |
2000年 | 2篇 |
1999年 | 2篇 |
1998年 | 2篇 |
1996年 | 2篇 |
1995年 | 1篇 |
1994年 | 1篇 |
1992年 | 1篇 |
1990年 | 1篇 |
1989年 | 1篇 |
1986年 | 1篇 |
排序方式: 共有188条查询结果,搜索用时 15 毫秒
51.
针对某型双加甲板拖网渔船导管桨,建立基于底拖网作业渔船工况和自航工况的综合性船、机、桨优化匹配模型,对船机桨进行多重比较优化。采用导管和大直径螺旋桨,并通过生产实践,验证优化设计的高效性,提高拖网渔船推进系统的效率,增大系柱的拖力。 相似文献
52.
53.
Hiroharu Kato Kento Miura Hajime Yamaguchi Masaru Miyanaga 《Journal of Marine Science and Technology》1998,3(3):122-129
The formation of air bubbles ejected through a single hole in a flat plate was observed in uniform flow of 2–10 m/s It was
confirmed that the size of the air bubbles was governed by main flow velocity and air flow rate. According to previous experiments,
the size of the bubbles is an important factor in frictional drag reduction by microbubble ejection. Usually bubbles larger
than a certain diameter (for example 1 mm) have no effect on frictional drag reduction. Three different methods were proposed
and tested to generate smaller bubbles. Among them, a 2D convex (half body of an NACA 64-021 section) with ejection holes
at the top was the best and most promising. The diameter of the bubbles became about one-third the size of the reference ejection
on a flat plate. Moreover, the bubble size did not increase with increasing flow rate. This is a favorable characteristic
for practical purposes. The skin friction force was measured directly with a miniature floating element transducer, and decreased
drastically by microbubble ejection from the top of the 2D convex shape. 相似文献
54.
55.
The motions of an infinitely long, two-dimensional runway subjected to the dynamic moving load imposed by an airplane taking
off are investigated. The runway is assumed to be floating in an inviscid fluid and is initially at equilibrium before the
plane takes off. The deformation of the runway resulting from the take-off is wave-like and moves in the same direction as
the plane. The maximum drag occurs when the plane catches up with the first wave. Three different runway configurations were
considered: a baseline and ones which were ten and one hundred times more flexible than the baseline. For these runways, the
added drag to the aircraft was very small, ranging from 1% for the stiffest to 10% for the most flexible runway. 相似文献
56.
57.
58.
59.
1吨级试验艇属于高密度中低速气垫船,其与气垫密度成平方关系的阻力峰值较大而设计推力相对较小,经采取措施解决了越峰困难问题。原阻力计算方法在阻力峰值处的计算结果不够精确是原因之一,故根据移动压力面兴波理论编制了直接计算兴波阻力的程序,使计算越峰所需推力更接近试验结果。理论计算与工程实践表明,在设计高密度中低速气垫船时需特别关注越峰性能校核,建议第一阻力峰处设计越峰裕度在原计算方法基础上应修正至不小于30%为宜。 相似文献
60.
利用计算流体力学软件Fluent开展动波壁圆柱绕流的数值计算,建立二维运动波浪壁圆柱模型。在来流速度u=0.005 m/s、雷诺数Re=500的情况下,开展动波壁波动速度c=0,0.005,0.01,0.015,0.02,0.025,0.03,0.04 m/s等8个工况的计算分析,并比较不同波动速度对流场结构、升力、阻力特性的影响。结果表明:动波壁圆柱能有效抑制流动的分离,消除交替脱落的尾涡,减阻效果突出;随着波动速度的增大,平均阻力系数呈明显下降趋势;当波速超过0.025 m/s时,阻力变为负值,即波动圆柱产生一定的推力。 相似文献