黄河大柳树坝址岩体破坏机制动力模拟试验分析

黄河黑山峡大柳树坝址区存在大范围的岩体松动破坏现象,其主要特征是岩体应力释放,结构面张开,密度显著下降。为进一步研究岩体松动的成因机制,在详细调查区域地质背景条件及区域地震动力作用基础之上,提出了地震动力作用与岩体松动现象的内在联系,通过动力模拟试验进一步证明大柳树坝址区存在的大深度、大范围岩体松动与历史上该地区发生的强烈地震具有密切关系。因此在目前的工程地质条件下,一旦发生较大强度的地震活动,坝址区所遭受的破坏程度会更大,对拟建的水利工程设施将产生严重威胁。

结构动力学模拟试验计算机测试系统现状及发展趋势

文章简要介绍了结构动力学模拟试验计算机测试系统的原理及技术演变过程,对该领域的技术现状及发展趋势作了探讨。

航天器动力学环境试验综合测试系统的设计

航天器在发射之前必须经过严格的地面条件验证;其中,航天器的动力学地面环境模拟试验对其顺利完成任务具有非常重要的意义;在航天器的动力学环境试验中,数据采集设备起着非常重要的作用,介绍了航天器动力学环境试验综合测试系统研制的目的、系统工作的原理、构成、硬件结构的研制以及解决的关键问题;最后的结果表明,这套系统完全可以满足航天器动力学地面试验的任务要求。

输水隧道动力模型试验中相似比尺规律的探讨

结构动力模型试验与动力模型破坏试验中,保持模型与原型相似的基本要求与处理技巧根据试验目的不同,而有所差别。这里就地下输水隧道考虑流-固耦合的动力模型试验进行理论研究和数值模拟,研究中根据工程的实际及模型试验选料的经济实用性,提出当原型与模型弹性模量不相等时的动力相似比尺是以围岩的弹性模量比来计算的规律。为今后复杂的地下水工结构动力模型的结构动力特性和破坏试验的相似问题拓宽思路,提供有用的参考价值。

考虑流-固耦合的输水隧道动力模型试验中的一种相似技巧

结构动力模型试验与动力模型破坏试验中,保持模型与原型相似的3种基本要求与处理技巧已在相关文献中提及。同时,也提及了对结构动力特性、弹性振动响应与破坏形态等试验目的不同,相似要求也有所差别,而这里将对地下软土中考虑流-固耦合的输水隧道的模型试验进行数值模拟研究。根据模型试验选料的经济实用性,提出了一种相似关系和技巧,并通过实例加以验证。数值模拟结果表明:在这种具体情况下,采用这种相似关系完全可以从模型试验的数据换算到原型,以便获得更多的有用信息,为今后地下输水工程模型试验的选材拓宽了思路,并提出了一些新的概念。

航天器动力学环境试验综合测试系统的设计思路

文章简要介绍了动力学环境模拟试验综合测试系统的原理、构成及关键技术,给出了大中型动力学综合测试系统硬件平台及应用软件系统的设计思路。

强震区岩体动力破坏机制研究

黄河黑山峡大柳树坝址区存在大范围的岩体破坏现象。在详细调查区域地质背景条件及区域地震动力作用基础之上,提出了地震动力作用与岩体破坏现象的内在联系,并通过动力模拟试验分析、证明了岩体破坏现象与历史上该地区发生的强烈地震有着密切关系。因此,在目前的工程地质条件下,一旦发生强度较大的地震活动,坝址区所遭受的破坏程度会更大,对拟建的水利工程设施将产生严重威胁。

FL-3风洞喷流试验高精度数字阀的设计与实现

详细介绍了FL-3风洞喷流、带涡轮动力模拟器(TPS)试验中用于流量和压力控制的数字阀系统的设计,包括技术指标、总体方案、通断阀门的类型和喷管的气动设计等。地面调试结果表明:数字阀系统设计合理,喷流流量绝对控制精度小于±5g/s,且控制时间快、效果平稳,满足了FL-3风洞喷流、TPS试验流量压力精确快速控制的设计指标。

Characterization of a Powertrain Test Bed in the Context of Virtual Validation of Drivability

Technological trends in the automotive industry toward a software-defined and autonomous vehicle require a reassessment of today’s vehicle development process.The validation process soaringly shapes after starting with hardware-in-the-loop testing of control units and reproducing real-world maneuvers and physical interaction chains.Here,the road-to-rig approach offers a vast potential to reduce validation time and costs significantly.The present research study investigates the maneuver reproduction of drivability phenomena at a powertrain test bed.Although drivability phenomena occur in the frequency range of most up to 30∙Hz,the design and characteristics substantially impact the test setup’s validity.By utilization of modal analysis,the influence of the test bed on the mechanical characteristic is shown.Furthermore,the sensitivity of the natural modes of each component,from either specimen or test bed site,is determined.In contrast,the uncertainty of the deployed measurement equipment also affects the validity.Instead of an accuracy class indication,we apply the ISO/IEC Guide 98 to the measurement equipment and the test bed setup to increase the fidelity of the validation task.In conclusion,the present paper contributes to a traceable validity determination of the road-to-rig approach by providing objective metrics and methods.

Simulation study of plane motion of air cushion vehicle

This research is on horizontal plane motion equations of Air Cushion Vehicle (ACV) and its simulation. To investigate this, a lot of simulation study including ACV's voyage and turning performance has been done. It was found that the voyage simulation results were accorded with ACV own characteristic and turning simulation results were accorded with USA ACV's movement characteristic basically.

Shaking table tests and numerical simulation of dynamic properties of underground structures

It is considered thai the damage of the underground structures caused by earthquakes is minor for a long time. However, the catastrophic damages induced by several recent earthquakes （e. g. Kobe earthquake in 1995 ） revealed that the study on the dynamic properties of the underground structures is indispensable. The dynamic behavior and damage mechanism of underground structure are analyzed by using shaking table tests （ both shallow-and deep-buried） and numerical simulation （3D FEM） including horizontal and vertical input motions, individually and simultaneously. From the results, the underground structure collapsed due to strong horizontal forces although vertical deformation is not negligible. The vertical excitation increases the response of structure, especially the stress and shear stress at the upper section; the soil influenced the property of soilstructure system. In the same excitation, the response in shallow-buried test is larger than deep case. Both overburden and vertical earthquake play important roles in the response of structure and those are two critical aspects in the design of the large-span underground structures, such as subway stations.

Internal heat transfer coefficients in microporous media with rarefaction effects

The internal heat transfer of different gases in microporous media was investigated experimentally and numerically.The experimental test section had a sintered bronze porous media with average particle diameters from 11 μm to 225 μm.The Knudsen numbers at the average inlet and outlet pressures of each test section varied from 0.0006 to 0.13 with porosities from 0.16 to 0.38.The particle-to-fluid heat transfer coefficients of air,CO 2 and helium in the microporous media were determined experimentally.The results show that the Nusselt numbers for the internal heat transfer in the microporous media decrease with decreasing the particle diameter,d p,and increasing Knudsen number for the same Reynolds number.For Kn>0.01,the rarefaction affects the internal heat transfer in the microporous media.A Nusselt number correlation was developed that includes the influence of rarefaction.The computational fluid dynamics(CFD) numerical simulation was carried out to do the pore scale simulation of internal heat transfer in the microporous media considering the rarefaction effect.Pore scale three-dimensional numerical simulations were also used to predict the particle-to-fluid heat transfer coefficients.The numerical results without slip-flow and temperature jump effects for Kn<0.01 corresponded well with the experimental data.The numerical results with slip-flow and temperature jump effects for 0.01<Kn<0.13 are lower than the numerical results without rarefaction effects,but closer to the experimental data.The numerical results with rarefaction effects can accurately simulate the unsteady heat transfer in the microporous media.

A miniature pump with a fluid dynamic bearing

This paper describes the development of a miniature pump having an impeller with an exit diameter of 24 mm supported with the motor rotor by a fluid dynamic beating. Tests verify that the miniature pump is stable and quiet for rotational speeds larger than 4000 rain-1. The three-dimensional turbulent flow in the entire pump flow passage and the laminar flow in the fluid dynamic bearing were then simulated numerically. The average pump performance was well predicted by the simulations. Both the tests and the simulations show that there is no obvious Reynolds effect for the miniature pump within the tested range of rotational speeds. The numerical results also show that the beating capacity of the fluid dynamic bearing increases with the pump rotor rotational speed and the eccentricity ratio of the journal to the bushing. This pump is very compact, so it is a prom- ising device for surgical use.

A method of magnetosonic characteristics to correct the "rarefaction shocks" problem arising in ZEUS

ZEUS is a magnetohydrodynamics simulation code widely used in astrophysical research.However,it was recently found that the code may produce artificial shocks in the rarefaction region in some numerical tests since it is not upwinded in fast and slow waves.We propose a method of magnetosonic characteristics to evolve compressional waves.The tests indicate that this method cures the "rarefaction shocks" problem to a large extent and it also greatly reduces some post shock oscillations.

Numerical Simulation of the Tip Aerodynamics and Acoustics Test

The application of an efficient flow control system on helicopter rotor blades may lead to improved aerodynamic performance. Recently, our invention of Rod Vortex Generators(RVGs) has been analyzed for helicopter rotor blades in hover with success. As a step forward, the study has been extended to forward flight conditions. For this reason, a validation of the numerical modelling for a reference helicopter rotor(without flow control) is needed. The article presents a study of the flow-field of the AH-1G helicopter rotor in low-, medium- and high-speed forward flight. The CFD code FLOWer from DLR has proven to be a suitable tool for the aerodynamic analysis of the two-bladed rotor without any artificial wake modelling. It solves the URANS equations with LEA(Linear Explicit Algebraic stress) k-ω model using the chimera overlapping grids technique. Validation of the numerical model uses comparison with the detailed flight test data gathered by Cross J. L. and Watts M. E. during the Tip Aerodynamics and Acoustics Test(TAAT) conducted at NASA in 1981. Satisfactory agreements for all speed regimes and a presence of significant flow separation in high-speed forward flight suggest a possible benefit from the future implementation of RVGs. The numerical results based on the URANS approach are presented not only for a popular, low-speed case commonly used in rotorcraft community for CFD codes validation but preferably for medium- and high-speed test conditions that have not been published to date.

Localization and shock waves in curved manifolds

The investigation of the interplay between geometry and nonlinearity may open the road to the control of extreme waves. We study three-dimensional localization and dispersive shocks in a bent cigar shaped potential by the nonlinear Schro¨ dinger equation. At high bending and high nonlinearity, topological trapping is frustrated by the generation of curved wave-breaking. Four-dimensional parallel simulations confirm the theoretical model. This work may contribute to novel devices based on geometrically constrained highly nonlinear dynamics and tests and analogs of fundamental physical theories in curved space.