• Journal of the Korean Society of Propulsion Engineers
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• v.17 no.5
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• pp.54-59
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• 2013

Micro shock tubes are now-a-days used for a variety engineering applications such as in the field of aerospace, combustion technology and drug delivery systems. But the flow characteristics of micro shock tube will be different from that of well established conventional macro shock tube under the influence of very low Reynolds number and high Knudsen number formed due to smaller diameter. In present study, experimental studies were carried out to a closed end (downstream) Micro Shock Tube with two different diameters were investigated to understand the flow characteristics. Pressure values were measured at different locations inside the driver and driven section. The results obtained show that with the increase in diameter the shock propagation velocity increases as well as the effect of reflected shock wave will be more significant under the same diaphragm rupture pressure.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.7
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• pp.33-39
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• 2005

A mathematical model, GUNBLAST, of blast waves emitted from a gun muzzle is established, and structural response analyses for the blast load are performed. The blast wave can be divided into two kinds of waves, free field and reflected blast waves. In this research, the free field blast wave model is established by the use of a scaling approach, and the reflected blast wave is calculated by using the oblique shock theory and computational fluid dynamic calculation. GUNBLAST is applied to two kinds of structural models. To investigate the effect of the muzzle distance from a structural surface, the blast waves on a plate for various muzzle distances are compared to uniform loads. Moreover, the transient response analysis of an aircraft wing model with a 12.7mm gun is carried out by using MSC/NASTRAN. From the results, it can be shown that the blast wave can cause broad random vibration and high frequency damage to equipments mounted in the aircraft.

• Journal of the Korean Society of Propulsion Engineers
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• v.25 no.6
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• pp.20-28
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• 2021

High enthalpy test facilities, such as a shock tunnel, are to be operated at the specific pressure ratio according to the desired test condition. A metallic diaphragm is machined or a forced rupture device is used to open it at a specific pressure ratio. The diaphragm opening procedure takes several hundred microseconds including rupture and deformation. This process is expected to affect the test conditions. In this study, numerical simulation was performed for different materials, thicknesses, and opening ratios. And the characteristics of shock wave generation and the stagnation condition in the tube are investigated. Results show that the final opening ratio and rupturing procedure directly affect the speed of a shock wave, stagnation pressure, and test time.

• 한국전산유체공학회:학술대회논문집
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• 1995.10a
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• pp.213-218
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• 1995

마하수 4일때 초음속 풍동의 벽면과 모델지지부의 간섭에 관해 연구하였다. 특히 모델지지부 주위에서의 충격파 형성과 sting, strut 그리고 second throat에서의 반사 충격파의 상호 작용에 연구의 촛점을 두었다. 수치 기법은 내재적 플럭스 차분 분할기법 (implicit flux-difference splitting technique)을 사용하였다. 2차원과 3차원 유동해석 결과로부터 모델지지부 후류의 유동에 미치는 diffuser 출구 경계조건의 영향을 알아보았다.

• Journal of computational fluids engineering
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• v.4 no.3
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• pp.35-43
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• 1999

In this study, the shock wave focusing of an elliptic reflector is numerically simulated by solving the Euler equations. The numerical method is the second order upwind TVD scheme with a finite volume discretization. For the verification of the present method, we simulate the moving shock wave passing through a two-dimensional corner. The computed isopycnics are compared with the earlier experiment. Numerical results of the elliptic reflectors show that the density and pressure at the focusing point increase linearly as the aspect ratio of the reflector becomes deep. On the other hand, the gas dynamic focal length decreased with the increase of the reflector aspect ratio.

• Proceedings of the KSME Conference
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• 2002.08a
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• pp.165-168
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• 2002

This paper describes the dynamics of the weak shock wave propagating inside some kinds of branched pipe bends. Computations are carried out by solving the two-dimensional, compressible, unsteady Euler Equations. The second-order TVD(Total Variation Diminishing) scheme is employed to discretize the governing equations. For computations, two types of branched pipe($90^{\circ}$ branch,$45^{\circ}$ branch) with a diameter of D are used. The incident normal shock wave is assumed at D upstream of the pipe bend entrance, and its Mach number is changed between 1.1 and 2.4. The flow fields are numerically visualized by using the pressure contours and computed schlieren images. The comparison with the experimental data performed for the purpose of validation of computational work. Reflection and diffraction of the propagating shock wave are clarified. The present computations predicted the experimented flow field with a good accuracy.

• Proceedings of the KSME Conference
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• 2001.11b
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• pp.456-461
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• 2001

This paper depicts the weak shock wave propagating inside some kinds of pipe bends. Computational work is to solve the two-dimensional, compressible, unsteady Euler Equations. The second-order TVD scheme is employed to discretize the governing equations. For the computations, the incident normal shock wave is assumed at the entrance of the pipe bend, and its Mach number is changed between 1.1 and 1.7. The turning angle and radius of the curvature of the pipe bend are changed to investigate the effects on the shock wave structure. The present computational results clearly show the shock wave reflection and diffraction occurring in the pipe bend. In particular, the vortex generation, which occurs at the edge of the bend, and its shedding mechanism are discussed in details.

• 한국가시화정보학회:학술대회논문집
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• 2002.11a
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• pp.113-116
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• 2002

The shock wave discharged from an annular duct leads to very complicated flow features, such as Mach stem, spherical waves, and vortex rings. In the current study, the merging phenomenon and propagation characteristics of the shock wave are numerically investigated using a CFD method. The Harten-Yee's total variation diminishing (TVD) scheme is used to the unsteady, axisymmetric, two-dimensional, compressible Euler equations. The Mach number of incident shock wave $M_s$ is varied in the range below 2.0. The computational results are visualized to observe the major features of the annular shock waves discharged from the tube. On the symmetric axis, the peak pressure produced by the shock wave and its location depend upon strongly the radius of the annular tubes. A Mach stem is generated along the symmetric axis of the annular tubes.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2007.12a
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• pp.163-165
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• 2007

제주 외항의 2단계 항만시설 사업으로 동방파제, 동방파호안, 접안시설, 친수호안, 접속호안 등 2,374m 구간에 대해 방파제 내파 안정성과 반사파 저감을 위한 단면계획을 통해 설계에 반영하였으며 지반 침하 및 지진피해 최소화를 위한 구조물의 사용 및 내구성을 중대시켰으며, 특히 크루저 선박의 본격취항을 대비한 친수공간개념의 도입에 많은 노력을 기울였다. 대상 사업지는 지형적 특성상 복잡한 형태의 고파랑이 작용하므로 방파제의 설계파를 7.3m로 상향조정하였고, 방파제 제간부에 발생하는 충격쇄파압에 대한 안정을 확보하기 위해 소파블록 피복케이슨제를 적용하였다. 제주도가 가지는 국제적 위상에 맞추어 국제미항개발, 레저형 웰빙공간조성 및 제주항이 가지는 자연적 특성을 반영하여 친수 방파제와 호안 및 배후시설의 친환경적인 배려를 최대화 하였다. 해양 생태계 보호를 위하여 해조류 서식지 및 해중림 조성 등 생태복원계획도 수립하였다.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1995.10a
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• pp.68-73
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• 1995

반사음이 포함된 신호의 계측을 통하여 원음의 크기와 반사계수의 크기, 지연시간 등의 추출을 수치적 예를 사용하여 규명해 보았다. 반사계수의 측정시, 폐쇄된 음장에서는 정상파비로 표시되는 단일 주파수 신호를 사용하는 것이 실제 계측시 가장 손쉬운 방법이며, 광역의 주파수 성분에 걸쳐 그 값을 파악할 필요가 있는 경우에는 켑스트럼 상에서 반사파의 효과가 원음과 확연히 구분되는 신호를 사용하는 것이 신호처리 과정에서 불필요한 부담을 제거시켜 준다. 개방 음장에서는 반사파가 1개 밖에 포함되지 않으므로 이 경우에는 PSD 상의데이터 처리를 통하든지 또는 캡스트럼의 재편집을 통하여 원음의 크기와 성분 그리고 반사계수 등을 손쉽게 추출해 낼 수 있다. 광대역 주파수 성분을 가진 음원을 계측에 사용할 경우에는 comb lifter의 적용에 보다 세심한 주의를 기울일 필요가 있으며 켑스트럼 상의 추가 충격응답함수의 식별에 보다 더 합리적인 방법이 강구되어야 할 것이다.