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991.
推导得到轴向极化的圆柱型正交各向异性压电弹性力学的三维状态方程,采用细分近似方法,得到了状态方程的解,并建立了圆柱壳内外表面边界量之间的传递关系,分析了内充可压缩流体的层合压电圆柱壳的自由振动问题,给出了频率方程的精确形式,并作了具体计算。 相似文献
992.
Chia-Shun Yih 《Acta Mechanica Sinica》1993,9(2):97-101
A general solution of the Boussinesq equation is presented which solves the problem of interaction of any number of right-going
and left-going solitary waves. The solution relies on the exact solution of Gardner, Greene, Kruskal, and Miura (1967), and
has the same degree of accuracy as that solution, but has a wider scope of application. It is much simpler than, but as accurate
as, Hirota's exact solution (1973) of the Boussinesq equation, to which the present solution is compared for the simplest
case of two solitary waves in head-on collision. 相似文献
993.
数值研究激波与旋涡的相互作用 总被引:4,自引:1,他引:4
从非定常形式的Euler方程出发,数值模拟了运动激波与旋涡相互作用的非定常流动过程。为保证激波具有较高的分辨率,采用对称型TVD格式进行了数值计算。结果表明。这样可以有效地模拟流场中一些复杂的流动现象,如激波变形、激波分叉和三波点的形成,以及旋涡结构的变化过程等,并与已有的实验流动显示相符良好。同时,也是对TVD格式求解这类问题的一次初步尝试。 相似文献
994.
The reflection and diffraction of a planar shock wave around a circular cylinder are a typical problem of the complex nonlinear
shock wave phenomena in literature. It has long been studied experimentally, analytically as well as numerically. Takayama
in 1987 obtained clear experimental pictures of isopycnics in shock tube under the condition that the impinging shock wave
propagates as far as 3 diameters away from the cylinder. To know more completely the whole unsteady process, it is desirable
to get experimental results in a region which is more than 10 diameters away from the cylinder. This is what has been done
in this paper by using the pulsed laser holographic interferometry for several shock Mach numbers of the impinging shock.
Results for several moments are shown, giving more knowledge about the whole unsteady flow field. This is useful for a reliable
and complete understanding of the changing force acting on the cylinder, and provides interesting data to check the performance
of many recently developed high resolution numerical methods for unsteady shock wave calculation.
The project suported partially by National Natural Science Foundation of China 相似文献
995.
996.
A computational study has been carried out to examine the effects of driver gas contamination in the NASA HYPULSE facility at GASL when operating with a detonation driver in reflected-shock tunnel mode. Unlike high-enthalpy shock tunnels which use helium as a driver gas, the driver gas in a detonation driver consists of a mixture of water vapour and argon, which has very different chemical and thermodynamic properties than those of helium. The purpose of the present work is to quantitatively evaluate the effects of driver gas contamination on the flow properties in the test section. Two computational analyses have been performed. The first analysis examined the nozzle flow under the influence of a prescribed level of driver gas contamination. In the second analysis, the transient development of the driver gas leakage in the reflected-shock region in the shock tube is studied. The unique flow features brought about by the detonation-driver gas and the method for detecting the contamination are discussed.Received: 6 August 2002, Revised: 22 September 2003, Published online: 10 February 2004Correspondence to: R.S.M. ChueAn abridged version of this paper was presented at the 23rd International Symposium on Shock Waves at Fort Worth, Texas, July 23 to 27, 2001 相似文献
997.
应用二种截然不同的炸药PBX 95 0 1和T2 ,计算了爆轰波在不同入射角下与金属平板的斜相互作用。在正规反射区 ,计算结果与激波极线理论基本一致 ;应用燃烧模型 ,分别计算了Fe球壳装药JB90 0 3(HE)及JB90 14 (IHE)散心爆轰波的绕射传播 ,计算结果与实验很好地符合。在非正规反射区 ,二维拉氏程序计算结果明显地不同于经典理论结果 ,计算中没有出现Mach反射。计算结果显示 ,毗邻介质影响节点附近的爆轰波阵面形状及爆轰波速度 ;不同的反应率函数计算的节点图像不同。 相似文献
998.
Tang Guiming 《Acta Mechanica Sinica》1998,14(2):139-146
An experimental study was conducted on shock wave turbulent boundary layer interactions caused by a blunt swept fin-plate
configuration at Mach numbers of 5.0, 7.8, 9.9 for a Reynolds number range of (1.0∼4.7)×107/m. Detailed heat transfer and pressure distributions were measured at fin deflection angles of up to 30° for a sweepback
angle of 67.6°. Surface oil flow patterns and liquid crystal thermograms as well as schlieren pictures of fin shock shape
were taken. The study shows that the flow was separated at deflection of 10° and secondary separation were detected at deflection
of ϑ≥20°. The heat transfer and pressure distributions on flat plate showed an extensive plateau region followed by a distinct
dip and local peak close to the fin foot. Measurements of the plateau pressure and heat transfer were in good agreement with
existing prediction methods, but pressure and heating peak measurements atM≥6 were significantly lower than predicted by the simple prediction techniques at lower Mach numbers.
The project supported by China Academy of Launch Vehicle Technology 相似文献
999.
The present work is devoted to the experimental and numerical study ofthe interaction of a turbulent plane jet with a rectangular cavity.Several flow regimes have been found to occur: the non-oscillationregime, the stable oscillation regime and an unstable oscillationregime. The first two regimes have been particularly considered. Theexperimental study has been carried out using hot wire anemometry andsome visualisations. The numerical predictions based on statisticalmodelling have been made using on the one hand the standard k– model and on the other hand a two-scales split spectrum model. The structuralproperties of the flow have been described for the different situations.For the oscillatory regime, a parametrical study allowed to determinethe influence of the jet exit location and the Reynolds number on thefrequency of the jet flapping. The one point closures have been able topredict the oscillatory regime, and in particular the two-scales modelled to improved results because better account is taken of lag effectsin unsteady non-equilibrium situations. 相似文献
1000.
Genta Kawaguchi Prof. Dr. Mitsuhiko Maesato Dr. Tokutaro Komatsu Prof. Dr. Hiroshi Kitagawa Prof. Dr. Tatsuro Imakubo Dr. Andhika Kiswandhi Dr. David Graf Prof. Dr. James S. Brooks 《Angewandte Chemie (International ed. in English)》2015,54(35):10169-10172
Simultaneous manipulation of both spin and charge is a crucial issue in magnetic conductors. We report on a strong correlation between magnetism and conductivity in the iodine‐bonded molecular conductor (DIETSe)2FeBr2Cl2 [DIETSe=diiodo(ethylenedithio)tetraselenafulvalene], which is the first molecular conductor showing a large hysteresis in both magnetic moment and magnetoresistance associated with a spin‐flop transition. Utilizing a mixed‐anion approach and iodine bonding interactions, we tailored a molecular conductor with random exchange interactions exhibiting unforeseen physical properties. 相似文献