• 대한기계학회논문집B
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• 제22권9호
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• pp.1229-1237
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• 1998

Experiments of shock-wave/turbulent boundary layer interaction were conducted by using a supersonic wind tunnel. Nominal Mach number was varied in the range of 1.6 to 3.0 by means of different nozzles. The objective of the present study is to investigate the effects of boundary layer suction on normal shock-wave oscillations caused by shock wave/boundary layer interaction in a straight duct. Two-dimensional slits were installed on the top and bottom walls of the duct to bleed turbulent boundary layer flows. The bleed flows were measured by an orifice. The ratio of the bleed mass flow to main mass flow was controlled below the range of 11 per cent. Time-mean and fluctuating wall pressures were measured, and Schlieren optical observations were made to investigate time-mean flow field. Time variations in the shock wave displacement were obtained by a high-speed camera system. The results show that boundary layer suction by slits considerably reduce shock-wave oscillations. For the design Mach number of 2.3, the maximum amplitude of the oscillating shock-wave reduces by about 75% compared with the case of no slit for boundary layer suction.

• 대한기계학회논문집
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• 제18권6호
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• pp.1582-1589
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• 1994

The characteristics Prandt1-Meyer expansion of supersonic flow with condensation through a wavy wall in a channel are investigated by experiment and numerical direct marching method of characteristics. In the present study, for the case of moist air flow in the type of indraft supersonic wind tunnel, the dependency of location of formation and reflection of the oblique shock wave generated by the wavy wall and the distribution of flow properties, on the specific humidity and temperature at the entrance of wavy wall and the attack angle of the wavy wall to the main stream is clarified by schlieren photograph, distribution of static pressure and Mach number, and plots of numerical results. Also, we confirm that the wavy wall plays an important key role in the formation of oblique shock wave, and that the effect of condensation on the flow field appears apparently.

• 한국가시화정보학회지
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• 제10권1호
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• pp.40-46
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• 2012

Recently micro shock tube is extensively being used in many diverse fields of engineering applications but the detailed flow physics involved in it is hardly known due to high Knudsen number and strong compressibility effects. Unlike the macro shock tube, the surface area to volume ratio for a micro shock tube is very large. This unique effect brings many complexities into the flow physics that makes the micro shock tube different compared with the macro shock tube. In micro shock tube, the inter- molecular forces of working gas can play an important role in specifying the flow characteristics of the unsteady shock wave flow which is essentially generated in all kinds of shock tubes. In the present study, a CFD method was used to predict and visualize the unsteady shock wave flows using the unsteady compressible Navier-Stokes equations, furnished with the no-slip and slip wall boundary conditions. Maxwell's slip equations were used to mathematically model the shock movement at high Knudsen number. The present CFD results show that the propagation speed of the shock wave is directly proportional to the initial pressure and diameter of micro shock tube.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2010년도 춘계학술대회 논문집
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• pp.433-434
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• 2010

• 한국지반공학회논문집
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• 제31권6호
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• pp.27-44
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• 2015

일정수심상에서 임의반사율을 갖는 부분중복파와 흐름이 공존하는 경우 얕은 두께를 포함한 유한두께 및 무한두께의 해저지반내에서 동적응답을 나타내는 해석해를 유도한다. 해석해에서 반사율이 0인 경우는 진행파와 흐름과의 공존장으로, 반사율이 1인 경우는 완전중복파와 흐름과의 공존장으로 간단히 변환된다. Biot의 압밀이론에 기초하여 해저지반은 투과탄성매체로, 간극유체는 압축성으로, 그리고 지반내 간극수의 흐름은 Darcy법칙으로 각각 가정된다. 도출된 해석해는 기존의 해석결과와의 비교 검토로부터 검증되며, 실제 계산에서는 반사율, 흐름속도, 입사파의 주기 및 지반두께 등의 변화에 따른 지반변위, 간극수압, 유효응력 및 전단응력의 변동특성을 면밀히 검토한다. 이로부터 흐름이 존재하는 경우 흐름으로 인한 입사파와 반사파의 주기 및 파장의 변화로 인하여 흐름이 없는 경우의 지반내 동적응답과는 큰 차이를 나타내며, 또한 반사율의 크기에 따라 동적응답에서 큰 차이가 나타난다는 것을 확인할 수 있다.

• 한국해안·해양공학회논문집
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• 제30권4호
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• pp.153-165
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• 2018

본 연구는 olaFlow을 이용하여 먼저 소스에 의한 불규칙파의 조파에서 목표주파수스펙트럼과 조파된 파랑의 주파수스펙트럼과의 비교 검토로부터 olaFlow의 타당성을 검증하였다. 이로부터 불규칙파랑 하 3차원투과성잠제를 대상으로 잠제 주변에서 형성되는 파고분포와 같은 수면변동의 특성과 설상사주의 주요외력으로 작용하는 평균유속, 연안류 및 난류운동에너지 등을 포함한 유속장의 특성을 수치적으로 검토하였다. 수치해석결과에 따르면 잠제 사이의 개구폭이 감소할수록 개구부 중앙에서는 자승평균평방근파고가 증가하지만 개구부 배후에서는 자승평균 평방근파고가 감소하며, 잠제의 개구폭이 넓을수록 강한 연안류가 형성됨과 동시에 수송유량이 증가되는 것을 확인할 수 있었다. 이로부터 잠제 배후에 형성되는 설상사주의 형성원인을 파악할 수 있었다.

• 한국해양공학회지
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• 제25권3호
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• pp.19-27
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• 2011

In case of constructing submerged breakwaters for the purpose of preventing coastal erosion, the number of submerged breakwaters, as well as their asymmetry is dependent on the field conditions. The aim of the present study was to examine the 3-D hydrodynamic characteristics (3-D wave field, wave height, mean water level, and mean flow) around the asymmetric submerged breakwaters using a 3-D numerical model, LES-WASS-3D, which was validated through a comparison with existing experimental data and showed fairly nice agreement. From the numerical results, the wave height, mean water level, and mean flow are discussed in relation with the variation in the breakwater length ratio.

• 한국해안·해양공학회논문집
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• 제30권4호
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• pp.166-179
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• 2018

본 연구는 파-흐름의 공존장에 설치된 3차원투과성잠제에 관해 흐름방향에 따라 변화되는 잠제 주변에서 파고분포와 같은 수면변동의 특성 및 설상사주의 주요외력으로 작용하는 평균유속, 연안류 및 난류운동에너지 등을 포함한 유속장의 특성을 수치적으로 검토하였다. 수치해석에는 오픈소스 CFD 코드인 olaFlow를 적용하였으며, 대상파랑은 규칙파와 불규칙파로 하였다. 수치해석결과로부터 흐름방향(순방향과 역방향)에 따른 잠제 제간부 배후에서 파고변화는 난류운동에너지와 밀접한 관계를 가지며, 흐름이 존재하는 경우는 흐름이 없는 경우보다 약한 연안류가 형성됨과 동시에 수송유량이 감소되는 것을 확인할 수 있었다. 이로부터 흐름의 유무 및 방향이 잠제 배후에 형성되는 설상사주의 형성과정에 미치는 영향을 파악할 수 있었다.

• Journal of Ship and Ocean Technology
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• 제4권3호
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• pp.33-45
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• 2000

A computational system for wave and viscous flow analysis (WAVIS) has been developed. The system includes a pre-processor, flow solvers and a post-processor. The pre-processor is composed of full form presentation, surface mesh and field grid generation. The flow solvers are for potential and viscous flow calculation. The post-processor has graphic utility for result analysis. All the programs are integrated in a GUI-launcher package. To validate the developed CFD programs of WAVIS, the calculated results for modern commercial hull forms are compared with measurements. It is found that the results from WAVIS are in good agreement with the experimental data, illustrating the accuracy of the numerical methods employed for WAVIS.

• 대한기계학회논문집B
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• 제23권2호
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• pp.234-242
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• 1999

Flow phenomena such as the pressure transients Inside a high-speed railway tunnel and the Impulsive waves at the exit of the tunnel are closely associated with the characteristics of the entry compression wave, which is generated by a train entering the tunnel. Tunnel entrance hood may be an effective means for alleviating the Impulsive waves and pressure transients. The objective of the current work is to explore the effects of the train nose shape and the entrance hood on the characteristics of the entry compression wave. Numerical calculations using the method of characteristics were applied to one-dimensional, unsteady, compressible flow field with respect to high-speed railway/tunnel systems. Two types of the entrance hoods and various train nose shapes were employed to reveal their influences on the entry compression wave for a wide range of train speeds. The results showed that the entry compression wave length increases as the train nose becomes longer and the train speed becomes lower. The entry compression wave length in the tunnel with hood becomes longer than that of no hood. Maximum pressure gradient in the compression wavefront reduces by the entrance hood. The results of the current work provide useful data for the design of tunnel entrance hood.