• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1996.04a
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• pp.246-252
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• 1996

본 연구는 아음속 충돌분류의 소음특성에 관한 연구로서 분류가 매끄러운 판(smooth plate)에 충돌 할 때 발생하는 충돌소음의 음압레벨, 지향성 그리고 음향파워 등을 구하기 위한 것이다. 연구방법은 Fig.1에서와 같이 노즐지름 d와 노즐과 평판과의 거리를 h라 할 때 노즐상류측에 있는 서지 탱크(surge tank)의 압력이 1.0atg에 도달한 상태에서 단계적으로 강하시키면서 h/d에 따른 충돌소음의 레벨을 측정하였다. 또한 탱크압력을 일정하게 유지시킨 상태에서 충돌소음의 지향성을 측정하고 음향파워를 계산하였다. 자유분류인 경우에도 같은 방법으로 측정하여 충돌음의 경우와 비교 고찰하였다.

• Transactions of the Korean hydrogen and new energy society
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• v.25 no.4
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• pp.449-458
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• 2014

The heat transfer phenomenon was investigated in this study when a single round water jet with the low velocity and against the direction of gravity flows to the downward facing Isothermal of definite thickness circular plate. Experimental investigation is performed for a single round jet diameter 4mm, 6mm, and 8mm with the jet velocity 2.4m/s and jet fluid temperature of $24^{\circ}C$, varied the ratio of nozzle clearance/nozzle diameter (H/D)1, 2, 3, 6, and 8, on circular plate isothermal condition with $85^{\circ}C$. The local convection heat transfer coefficient distributions are analyzed based on the visualization of jet flow field. The effects of the diameter of Nozzle, the ratio of H/D and the ratio of nozzle diameter/circular plate diameter on heat transfer phenomenon are investigated. As a results of experiment is obtained correlation equation, $Nu_r=3.18Re_r^{0.55}Pr_r^{0.4}$.

• Transactions of the Korean Society of Automotive Engineers
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• v.10 no.1
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• pp.9-16
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• 2002

The particles velocity in the instantaneous flow field and velocity change of particles along the jet centerline for various particle diameter in a circular turbulent impingement jet are investigated by using particle image velocimetry(PIV) and an equation of particle motion simplified by terms of inertia forces, drag and gravitational force. The jet Reynolds number was 3300 and 8700, and glass beads of 30,58 and 100$\mu$m in diameter were used. The PIV results show that the direction and size of velocity depends not only on the number density of particle but also on the particle momentum. The results obtained form calculation suggest that the particle velocity near the first impingement region deviated from local air velocity, which accords well with the PIV results. The rebound height of particle increase with the particle diameter. In the second-impingement, particle velocities increased sluggishly with Re=3300 but particle velocities uniformed with Re=8700 in stagnation region.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2008.04a
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• pp.383-388
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• 2008

A modeling method for the impact analysis of plate structures employing Hertzian contact theory is presented in this paper. Since local deformation as well as bending deflection of the plate occurs due to the collision, it has to be considered for the impact analysis. When the coefficient of restitution is employed for the impact analysis, the local deformation is not considered. For more accurate and reliable impact analysis, however, the local deformation should be considered. The effects of the location of collision and the collision mass on the impact duration time and the contact force magnitude are investigated through numerical studies employing Hertzian contact theory.

• Proceedings of the KSME Conference
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• 2008.11b
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• pp.2798-2803
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• 2008

The confined slot air jet impinging normally on a moving flat surface has been investigated numerically by using commercial CFD code Ansys CFX-V11. Turbulent flows are modeled using k-w turbulence model. Two-dimensional turbulent flow is considered. Calculations were conducted for a nozzle-to-plate spacing of eight slot nozzle width, at three Reynolds number(Re=4500, 6700 and 10,000) and four surface-to-velocity ratios i.e. 0, 0.25, 0.5 and 1. Results are compared against corresponding cases for heat transfer from a stationary plate. Local Nusselt number is calculated under constant wall temperature condition. The analysis reveals that the average Nusselt number increases considerably with the jet exit Reynolds number, but decrease with the plate velocity.

• Composites Research
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• v.22 no.2
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• pp.18-23
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• 2009

Failure of Kevlar29/Phenolic composite plate under high velocity impact of FSP(Fragment Simulation Projectile) is investigated using a non-linear explicit finite element code, LS-DYNA. Composite laminate and impactor are idealized by solid element and interface between laminas are modeled by tied-break element in LS-DYNA. Interaction between impactor and laminate is simulated face-to-face eroding contact algorithm. When the stress level meets a failure criteria, the layer in the element is eroded. Numerical results are verified by existing test results.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.4
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• pp.79-84
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• 2005

An experimental investigation for impingement of under-expanded, axisymmetric jets on a flat plate has been conducted, and the surface pressure, the adiabatic wall temperature distributions on the plate have been measured in detail. For the explanation on the wall temperature distributions, the total temperature distributions along a free jet have also been measured with total temperature probes. In this study, the under-expansion ratio and the nozzle-to-plate distance have been considered as experimental parameters. Depending on nozzle-to-plate distances, different distributions of adiabatic wall temperature are shown by the energy separation at a jet edge and a impinged surface. Also, the recovery factor on a stagnation point decreases significantly due to the isolation of fluid particles in a central region.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2016.11a
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• pp.108-108
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• 2016

마그네트론 스퍼터링은 박막의 증착에 널리 사용되는 기술로 음극의 설계가 핵심적이다. 영구 자석과 전자석을 겸용하는 경우도 있고 고주파 코일을 추가하여 2차 플라즈마 발생을 유도하여 공정의 유연성을 한층 높인 방법도 오랫동안 사용되어 왔다. 전자의 자기장 하에서의 운동은 Lorentz force를 적분하여 예측할 수 있으며 가장 중요한 전자 - 중성간의 충돌 과정인 탄성 충돌, 여기 충돌, 이온화 충돌을 고려하면 보다 실질적인 마그네트론 플라즈마의 거동을 이해하고 그 결과를 기반으로 자석 배치를 설계할 수 있다. PIC (particle-in-cell) code를 이용하면 플라즈마 내의 전자기장 효과를 상세히 검증해볼 수 있지만 계산 시간의 부담 때문에 고성능 병렬 컴퓨터를 사용하여야 한다. 그 이유는 하전입자(전자, 이온)의 공간적인 분포에 변화가 발생하면 전위가 영향을 받고 전자의 가속이 발생하는 쉬스(sheath)의 두께가 따라서 변화하기 때문이다. 여기서 계산 시간의 단축을 위한 가정, 즉, 쉬스의 두께가 일정하다는 사실을 적용하면 계산시간을 획기적으로 단축 시킬 수 있으며 병렬 계산의 효율성도 향상시킬 수 있다. 본 연구에서는 이와 같은 원리에 입각한 코드를 개발하고 평판 디스플레이용 사각형 음극에 대해서 적용했던 경험을 바탕으로 원형의 스캔형 마그네트론 음극 구조의 이해와 설계에 적용하고자 코드를 개발하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2000.11a
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• pp.31-31
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• 2000

초음속 충돌제트(impinging jet)의 열 및 운동량 전달(heat and momentum transfer)은 로켓의 이ㆍ착륙, 다단 로켓의 분리, 로켓의 방향조절을 위해 배기 노즐에 부착되는 제트 베인(jet vane)이나 스포일러 탭(spoiler tab), 수직/단거리 이착륙기의 발진, 미사일 발사시스템, 전투기 동체, 날개, 후미 부분에서 발사되는 미사일의 배기가스가 주변장치 등에 충돌할 때 발생되는 문제점 등을 사전 예측하여 관련장비의 설계 둥에 유용한 자료로 이용된다. 따라서 이에 대한 기초 연구로서 초음속 유동 실험장치를 이용하여 마하수(Mach Number) 1.0 및 1.8인 경우에 대하여 수직/경사평판에서 팽창 비, 거리, 경사각에 따른 충돌 면에서의 단열 벽면온도를 측정하였다. (중략)

• Proceedings of the KSME Conference
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• 2000.11b
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• pp.87-92
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• 2000

This study is to investigate the heat transfer characteristics the for a round turbulent jet impinging on the flat plate with and without rib. Liquid crystal/transient method was used to determine the Nusselt number distributions along the surface. The temperature on the surface was measured using liquid crystal and a digital color image processing system. The experiments were made fur the jet Reynolds number (Re) 23,000, the dimensionless nozzle-to-surface distance (L/d) from 2 to 10, and the rib type [height ($d_1$) 2mm, pitch (p) from 12 to 36mm]. It was found that for $L/d{\ge}6$ the average Nusselt numbers on the flat plate with rib type C ($p/d_1=16$) are higher than those without rib, mainly due to an increase in the turbulent intensity caused by flow separation, recirculation and reattachment on the wall surface.