• Geomechanics and Engineering
• /
• 제19권2호
• /
• pp.179-191
• /
• 2019

Based on the effective stress principle, a new formula for shear strength of unsaturated soil is derived under the general nonlinear Mohr-Coulomb (M-C) strength criterion to improve the classical strength criterion of unsaturated soil. Meanwhile, the simple irrigation model under steady seepage is adopted to obtain the distribution of the matrix suction or the degree of saturation (DOS) above the groundwater table in the slope. Then, combined with the improved strength criterion of unsaturated soil and the simple irrigation model under steady seepage, the limit equilibrium (LE) solutions for the unsaturated slope stability are established according to the global LE conditions of the entire sliding body with assumption of the stresses on the slip surface. Compared to the classical strength criterion of unsaturated soil, not only the cohesion soil but also the internal friction angle is affected by the matric suction or the DOS in the improved strength criterion. Moreover, the internal friction angle related to the matric suction has the nonlinear characteristics, particularly for a small of the matric suction. Thereafter, the feasibility of the present method is verified by comparison and analysis on some slope examples. Furthermore, stability charts are also drawn to quickly analyze the unsaturated slope stability.

• 지질공학
• /
• 제18권4호
• /
• pp.447-457
• /
• 2008

절리면의 거칠기, 충전물 등의 공학적 특성과 활동면 경사, 수압하중을 고려하여 암반사면의 파괴거동을 고찰하고 파괴시기를 예측하기 위하여 모형실험이 수행되었다. 절리면 거칠기는 폭, 길이, 높이 등을 고려하여 톱니형으로 제작하였다. 충전물은 거칠기의 돌출부 높이에 대하여 일정한 충전물두께를 유지하는 방식으로 0에서 돌출부 높이의 1.2배까지 증가시켰다. 수압증가에 따른 사면의 거동양상을 파악하기 위해서는 인장균열에 완전히 가해질 수 있는 수압을 100%로 하여 0.5%/min 및 1%/min의 속도로 0%에서 파괴 시 까지 수압하중을 증가시켰다. 모형실험은 활동면 경사각 $30^{\circ}$와 $35^{\circ}$에서 각각 거칠기, 충전물 두께, 수압하중증가 등의 조합을 변화시키면서 총 50회 수행하였다. 모형실험결과 절리면의 거칠기가 없는 경우의 파괴거동 양상은 수압하중 증가 조건과 충전물의 유무에 관계없이 선형 변위거동으로 나타나는 것이 특징적이다. 거칠기가 존재할 경우에는 충전물 두께가 거칠기 높이보다 낮을 때 계단형 변위거동이, 거칠기 높이 이상일 때 지수형 변위거동이 특징적이다. 이는 충전물 두께가 거칠기의 높이를 넘어서면 절리면의 거동특성이 충전물의 공학적 특성에 좌우되기 때문인 것으로 판단된다. 파괴를 유발하는 수압하중의 크기는 절리면의 거칠기가 증가함에 따라 증가한다. 충전물의 두께가 증가할수록 거칠기의 영향이 작아져 파괴 시 수압하중은 감소한다 파괴가 임박한 시점에서 3차 크립 형태의 변위거동을 보이는 지수형의 경우에는 inverse velocity를 이용한 파괴시기 예측이 가능한 것으로 판단된다. 다만 실험에서 나타난 거동특성이 완전한 지수형이 아니고 계단형과 지수형의 중간형태로 나타나는 경우가 대부분이므로 정확한 파괴시기 예측을 위해서는 다수에 걸친 파괴시간 추정이 필요할 것으로 사료된다.

• Tribology and Lubricants
• /
• 제33권3호
• /
• pp.92-97
• /
• 2017

The understanding of the friction characteristics of micro-textured surface is of great importance to enhance the tribological properties of nano- and micro-devices. We fabricate rectangular patterns with submicron-scale structures on a Si wafer surface with various pitches and heights by using a focused ion beam (FIB). In addition, we fabricate tilted rectangular patterns to identify the influence of the tilt angle ($45^{\circ}$ and $135^{\circ}$) on friction behaviour. We perform the friction test using lateral force microscopy (LFM) employing a colloidal probe. We fabricate the colloidal probe by attaching a $10{\pm}1-{\mu}m$-diameter borosilicate glass sphere to a tipless silicon cantilever by using a ultraviolet cure adhesive. The applied normal loads range between 200 nN and 1100 nN and the sliding speed was set to $12{\mu}m/s$. The test results show that the friction behavior varied depending on the pitch, height, and tilt angle of the microstructure. The friction forces were relatively lower for narrower and deeper pitches. The comparison of friction force between the sub-micro-structured surfaces and the original Si surface indicate an improvement of the friction property at a low load range. The current study provides a better understanding of the influence of pitch, height, and tilt angle of the microstructure on their tribological properties, enabling the design of sub-micro- and micro-structured Si surfaces to improve their mechanical durability.

• 대한조선학회논문집
• /
• 제53권5호
• /
• pp.343-352
• /
• 2016

In this study, a pre-swirl duct for the 180,000 DWT bulk carrier has been designed from a propulsion standpoint using CFD. The stern duct - designed by NMRI - was selected as the initial duct. The objective function is to minimize the value of delivered power in model scale. Design variables of the duct include duct angle, diameter, chord length, and vertical and horizontal displacements from the center. Design variables of the stators are blade number, arrangement angle, chord length, and pitch angle. A parametric design was carried out with the objective function obtained using CFD. Reynolds averaged Navier-Stokes equations have been solved; and the Reynolds stress model applied for the turbulent closure. A double body model is used for the treatment of free-surface. MRF and sliding mesh models have been applied to simulate the actuating propeller. A self-propulsion point has been obtained from the results of towing and self-propelled computations, i.e., form factor obtained from towing computation and towing forces obtained from self-propelled computations of two propeller rotating speeds. The reduction rate of the delivered power of the improved stern duct is 2.9%, whereas that of the initial stern duct is 1.3%. The pre-swirl duct with one inner stator in upper starboard and three outer stators in portside has been designed. The delivered power due to the designed pre-swirl duct is reduced by 5.8%.

• 대한조선학회논문집
• /
• 제56권4호
• /
• pp.373-382
• /
• 2019

This paper shows numerical results for the estimation of the propulsor efficiency of Pre-Swirl Duct for 176k bulk carrier as well as its design method. Reynolds averaged Navier-Stokes equations have been solved and the k-epsilon model applied for the turbulent closure. The propeller rotating motion is determined using a sliding mesh technique. The design process is divided into each part of Pre-Swirl Duct, duct and Pre-Swirl Stator. The design of duct was performed first because it is located further upstream than Pre-Swirl Stator. The distribution of velocity through the duct was analyzed and applied for the design of Pre-Swirl Stator. The design variables of duct include duct angle, diameter, and chord length. Diameter, chord length, equivalent angle are considered when designing the Pre-Swirl Stator. Furthermore, a variable pitch angle stator is applied for the final model of Pre-Swirl Duct. The largest reduction rate of the delivered power in model scale is 7.6%. Streamlines, axial and tangential velocities under the condition that the Pre-Swirl Duct is installed were reviewed to verify its performance.

• 한국유체기계학회 논문집
• /
• 제15권3호
• /
• pp.19-24
• /
• 2012

Propeller shall have high efficiency and improved aerodynamic characteristics to get the thrust to fly at high speed for the turboprop aircraft. That is way Clark-Y airfoil which is used to conventional 1600kW class aircraft propeller is selected as a blade airfoil. Adkins method is used for aerodynamic design and performance analysis with respect to the propeller design point. Adkins method is based on the vortex-blade element theory which design the propeller to satisfy the condition for minimum energy loss. propeller geometry is generated by varying chord length and pitch angle at design point of turboprop aircraft. The propeller design results indicate that is evaluated to be properly constructed, through analysis of propeller aerodynamic characteristics using the Meshless method and MRF, SM method.

• 한국진공학회:학술대회논문집
• /
• 한국진공학회 2012년도 제43회 하계 정기 학술대회 초록집
• /
• pp.123-123
• /
• 2012

초소수성 표면은 150도 이상의 높은 물 접촉각과 10도 이하의 낮은 sliding angle을 가지며 self-cleaning, anti-contamination 기능을 갖고 있는 것이 특징이다. 재료표면의 친수성과 소수성을 제어하기 위해서는 화학적 인자인 물질의 표면에너지나 물리적 인자인 표면 거칠기를 조절하는 방법이 있다. 초소수성 표면을 구현하기 위해서는 표면의 거칠기를 증가시키거나 표면 에너지를 낮춰야 하는데 고체 표면의 거칠기를 증가시키기 위해서는 일반적으로 표면에 microscale과 nanoscale의 계층구조를 형성시키는 방법이 사용된다. 자연계에 매우 풍부하게 존재하는 실리카는 내구성과 내마모성, 화학적 안정성, 고온 안정성 등을 지니고 있으며 인체에 무해하기 때문에 다양한 종류의 전자기기 및 부품의 내외장 코팅에 적용이 검토되고 있다. 이러한 관점에서 본 연구에서는 초소수성 코팅층을 구현하는 하나의 방법으로서 졸-겔방법으로 실리카 졸을 합성하여 전기분무법을 사용하여 microscale의 실리카 입자 코팅층을 형성하였으며, 표면 미세구조 조절 및 계층구조 형성과 불소화처리 공정을 통하여 초소수성 실리카 코팅층을 제조하였다. 이러한 초소수성 실리카 코팅층의 표면거칠기, 자외선 영향향, 내구성 등을 초소수성 관점에서 평가하였다.

• 한국소성가공학회:학술대회논문집
• /
• 한국소성가공학회 1992년도 춘계학술대회 논문집 92
• /
• pp.11-26
• /
• 1992

In this research, a numerical algorithm has been developed, which can be applied to the large deformation and large displacement contact problems between angle change have been proposed considering the change in geometric shape and rate of contact force. A set of linear simultaneous equations is constructed by adding the geometric shape change and contact conditions to the original stiffness matrix. A new method to determine time increment has been proposed based on Euler method, in which the condition to prevent the contact bodies from penetrating and overrunning each other has been taken into consideration. Practical application to contact problem is extrusion in which bodies are sliding along the contact boundary.

• 한국지반공학회:학술대회논문집
• /
• 한국지반공학회 2006년도 추계 학술발표회
• /
• pp.229-240
• /
• 2006

Most of rock slopes contain a lot of discontinuities which have a specific direction and various characteristics. In general, the collapses of the rock slopes occur when the sliding dip of the discontinuity is higher than the internal friction angle and also smaller than the free-air plane of the slope. If a general slope theory is only considered in the case of field exploration of the slopes, there is a possibility that dangerous slopes might be estimated as stable slopes. We mention problems that can easily fail to notice something in field exploration and propose the alternatives to solve the problems through the case studies.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2007년도 춘계학술대회A
• /
• pp.1126-1131
• /
• 2007

This paper presents unified chassis control (UCC) to improve the vehicle lateral stability. The unified chassis control implies combined control of active front steering (AFS), electronic stability control (ESC) and continuous damping control (CDC). A direct yaw moment controller based on a 2-D bicycle model is designed by using sliding mode control law. A direct roll moment controller based on a 2-D roll model is designed. The computed direct yaw moment and the direct roll moment are generated by AFS, ESP and CDC control modules respectively. A control authority of the AFS and the ESC is determined by tire slip angle. Computer simulation is conducted to evaluate the proposed integrated chassis controller by using the Matlab, simulink and the validated vehicle simulator. From the simulation results, it is shown that the proposed unified chassis control can provide with improved performance over the modular chassis control.