全文获取类型
收费全文 | 186篇 |
免费 | 37篇 |
国内免费 | 16篇 |
专业分类
化学 | 18篇 |
力学 | 105篇 |
数学 | 14篇 |
物理学 | 102篇 |
出版年
2023年 | 1篇 |
2022年 | 4篇 |
2021年 | 5篇 |
2020年 | 4篇 |
2019年 | 3篇 |
2018年 | 5篇 |
2017年 | 5篇 |
2016年 | 4篇 |
2015年 | 5篇 |
2014年 | 5篇 |
2013年 | 14篇 |
2012年 | 10篇 |
2011年 | 17篇 |
2010年 | 18篇 |
2009年 | 14篇 |
2008年 | 12篇 |
2007年 | 17篇 |
2006年 | 15篇 |
2005年 | 11篇 |
2004年 | 14篇 |
2003年 | 10篇 |
2002年 | 7篇 |
2001年 | 7篇 |
2000年 | 8篇 |
1999年 | 1篇 |
1998年 | 2篇 |
1997年 | 3篇 |
1996年 | 5篇 |
1995年 | 3篇 |
1994年 | 2篇 |
1992年 | 2篇 |
1991年 | 1篇 |
1990年 | 1篇 |
1986年 | 1篇 |
1985年 | 2篇 |
1983年 | 1篇 |
排序方式: 共有239条查询结果,搜索用时 250 毫秒
11.
应用边界层积分法,研究锥形喷嘴入口区域中湍动涡流的发展.球面坐标系中的控制方程,通过边界层的假定得到简化,并对边界层进行了积分.应用4阶Adams预测校正法求解该微分方程组.入口区域的切向和轴向速度,分别应用自由涡流和均匀速度分布来表示.由于缺乏收缩喷嘴中涡流的实验数据,需要用数值模拟对该发展模式进行逆向验证.数值模拟的结果证明,该解析模型在预测边界层参数中的能力,例如边界层的生长、剪切率和边界层厚度,以及不同锥度角时的涡流强度衰减率等.为所提出的方法引进一个简明而有效的程序,用以研究几何形状收缩设备内的边界层参数. 相似文献
12.
When the stagnation temperature of a perfect gas increases, the specific heats and their ratio do not remain constant any
more and start to vary with this temperature. The gas remains perfect and its state equation always remains valid, except
it will be called a calorically imperfect gas. The aim of this research is to develop the relations of the necessary thermodynamics
and geometrical ratios and to study the supersonic flow at high temperature (lower than the threshold of dissociation). The
results are found by the resolution of nonlinear algebraic equations and integration of complex analytical functions where
the exact calculation is impossible. The dichotomy method is used to solve the nonlinear equation, and the Simpson algorithm
is used for the numerical integration of the found integrals. A condensation of the nodes is used, since the functions to
be integrated have a high gradient at the extremity of the interval of integration. A comparison is made with a calorifcally
perfect gas to determine the error of this. An application is made for air in a supersonic nozzle.
The text was submitted by the authors in English. 相似文献
13.
Hirokazu Sato Shusaku Hamada Roberto M. Sertkawa Tatsuya Nishimura Takashi Usui Hideo Sekino 《高压研究》2013,33(1-6):403-413
Abstract Continuous flames have been observed in Supercritical water oxidation (scWO) of isopropyl alcohol (IPA), using a vertical continuous reactor with sapphire windows and a mixing nozzle. Two types of continuous flame were confirmed: the one was long pale blue colored and the other was red short cone shaped, changing blue to red at around air ratio 2.0. The flame was strongly influenced by IPA concentration, air ratio and design of the mixing nozzle. Results for decomposition of PA are presented for IPA concentrations ranging from 600 up to 28260 ppm as TOC and initial reactor temperatures, were mostly around 490°C, at 25 MPa. Decomposition rate at steady state was over 99.9%. Experimentally measured CO2 and O2 concentrations at the flue gas were in good agreement with theoretically calculated values. Even for low air ratio as 1.1, high decomposition rate without CO, NO, NO2 was achieved. 相似文献
14.
A numerical study has been carried out to investigate the gas flows in a micronozzle using a continuum model under both slip and no‐slip boundary conditions. The governing equations were solved with a finite volume method. The numerical model was validated with available experimental data. Numerical results of exit thrust showed good agreement with experimental data except at very low Reynolds numbers. For parametric studies on the effect of geometric scaling, the nozzle throat diameter was varied from 10 to 0.1 mm, whereas throat Reynolds number was varied from 5 to 2000. A correlation has also been developed to calculate the specific impulse at specified throat diameter and Reynolds number. The effect of different gases on the specific impulse of the nozzle, such as helium, nitrogen, argon and carbon dioxide, was also examined. Copyright © 2008 John Wiley & Sons, Ltd. 相似文献
15.
V. N. Zaikovskii S. P. Kiselev V. P. Kiselev 《Journal of Applied Mechanics and Technical Physics》2005,46(5):670-676
Large-scale streamwise vortices in the vicinity of a perforated wall in the supersonic part of the nozzle are studied. The governing effect of gas inflow through a perforated wall on origination and parameters of streamwise vortices is experimentally established.__________Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, Vol. 46, No. 5, pp. 68–75, September–October, 2005. 相似文献
16.
17.
Two problems are considered: the design of a supersonic nozzle with a uniform exit characteristic and the design of a subsonic nozzle part with a plane (straight) sonic line in the minimum cross section. It is shown how the choice of a nozzle profile approximation affects the direct solutions to variational gas dynamics problems. The nozzle profile is described by polynomials or splines (quadratic, cubic, rational). The varied variables are the profile’s expansion coefficients in terms of basis functions or the parameters to be interpolated. It is shown that a priori information on the monotonicity of the desired profile improves the efficiency of the solution. 相似文献
18.
喷嘴在分层注入过程中起到调节聚合物分子量和压力损失的作用,而多级喷嘴的结构,由于分子链的逐级剪切作用,可在保证注入粘度的同时,更大的减小压力的损失.在此基础上提出变直径多级喷嘴的几何结构,利用Fluent数值模拟软件,对单级喷嘴、等直径多级喷嘴进行数值模拟,分析不同结构喷嘴对三元复合溶液速度、压力、湍动能以及平均应变速率的影响,结果表明随着流量的增大,三种结构喷嘴的压力损失和平均应变速率均增大,合理的变直径串联喷嘴可以达到与等直径串联喷嘴相同的注入效果,同时尺寸较小,方便工程应用. 相似文献
19.
水煤浆喷嘴热冲蚀磨损机理研究 总被引:4,自引:5,他引:4
采用1Crl8Ni9Ti不锈钢、YG8硬质合金和Al2O3/(W,Ti)C陶瓷3种材料制备了水煤浆喷嘴,考察了其在水煤浆雾化和燃烧过程中的热冲蚀磨损机理.结果表明:喷嘴材料的硬度对水煤浆喷嘴的热冲蚀磨损行为具有重要影响;在相同条件下,高硬度的Al2O3/(W,Ti)C陶瓷喷嘴的冲蚀率最低,YG8硬质合金次之,硬度较低的1Crl8Ni9Ti不锈钢喷嘴的冲蚀率最高;在热冲蚀磨损工况下,1Crl8Ni9Ti不锈钢水煤浆喷嘴主要呈现微切削特征,YG8硬质合金水煤浆喷嘴主要呈现晶粒剥落特征,而Al2O3/(W,Ti)C陶瓷水煤浆喷嘴主要呈现研磨损伤和热崩特征. 相似文献
20.
This study investigates the experimentally observed hysteresis in the mean flow field of an annular swirling jet with a stepped‐conical nozzle. The flow is simulated using the Reynolds‐averaged Navier–Stokes (RANS) approach for incompressible flow with a k–ε and a Reynolds stress transport (RSTM) turbulence model. Four different flow structures are observed depending on the swirl number: ‘closed jet flow’, ‘open jet flow low swirl’, ‘open jet flow high swirl’ and ‘coanda jet flow’. These flow patterns change with varying swirl number and hysteresis at low and intermediate swirl numbers is revealed when increasing and subsequently decreasing the swirl. The influence of the inlet velocity profile on the transitional swirl numbers is investigated. When comparing computational fluid dynamics with experiments, the results show that both turbulence models predict the four different flow structures and the associated hysteresis and multiple solutions at low and intermediate swirl numbers. Therefore, a good agreement exists between experiments and numerics. Copyright © 2006 John Wiley & Sons, Ltd. 相似文献