• 대한조선학회논문집
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• 제32권1호
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• pp.118-131
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• 1995

수중폭발을 받게 되는 해군 함정이나 충격하중을 받게 되는 초고속선의 구조에 대한 내충격 파손해석을 거시해석(global or macro analysis)과 미시해석(fine or micro analysis)의 두 단계로 나누어 수행하였다. 거시해석은 이중근사기법(DAA : Doubly Asymptotic Approximation)을 이용하였다. 심한 충격하중을 받는 구조는 주로 세 가지 파괴모드를 나타내는데 이는 충격후기에 주로 나타나는 동소성좌굴(Dynamic plastic buckling)에 기인하는 소성대변형과 충격초기에 주로 나타나는 인장 파괴(Tensile tearing failure)와 횡전단파괴(Transverse shear failure)가 있다. 본 논문의 미시해석에서는 잠수구조의 종보강재에 충격압력이 가해진 경우에 대하여 응력파(stress wave)의 파급과 이 응력파와 균열과의 상호작용에 의한 동적응력강도계수 $K_I(t)$의 계산함으로써 인장 파괴모드(Tensile tearing failure mode)해석을 수행하였다. 특히, 동적응력강도계수 $K_I(t)$의 계산에 있어서 실험적 방법으로 널리 사용되는 shadow optical method of caustic로부터 개발된 numerical caustic method를 사용하였다. 본 논문의 충격파손해석 수치 예로서 해석모델을 완전잠수주상체로 잡고 거시해석을 수행한 후 이로부터 구한 충격압력을 입력자료로 하여 종보강재에 대하여 미시해석을 수행하였다.

• 한국전자파학회논문지
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• 제30권2호
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• pp.173-176
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• 2019

본 논문에서는 밀리미터파 탐색기에 적용 가능한 Ka-대역 도파관 로터리조인트를 설계 및 제작하였다. 제안된 로터리 조인트는 낮은 정재파 비와 저손실 특성을 유지하며, 방위각과 고각 회전이 가능하도록 하는 두 개의 회전축으로 설계되어 있다. 또한 구형 도파관과 원형 도파관 사이에 전파 모드를 정합하기 위한 리지 도파관 형태의 모드 변환기와 ${\lambda}/4$ 길이의 초크 구조로 로터리 조인트를 설계하였다. 제작된 로터리 조인트의 성능은 회로망 분석기와 고출력 송신기를 이용하여 확인하였으며, 진동/충격 시험을 통해 신뢰성 검사를 수행하였다. 그 결과, 중심 주파수$(F_C){\pm}500MHz$의 대역에서 최대 정재파비 1.19 : 1 이하, 삽입손실 0.80 dB 이하의 우수한 특성을 갖는 것을 확인하였다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 추계학술대회
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• pp.490-495
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• 2003

In steel-making process of iron and steel industry, the purity and quality of steel can be dependent on the amount of CO contained in the molten metal. Recently, the supersonic oxygen jet is being applied to the molten metal in the electric furnace and thus reduces the CO amount through the chemical reactions between the oxygen jet and molten metal, leading to a better quality of steel. In this application, the supersonic oxygen jet is limited in the distance over which the supersonic velocity is maintained. In order to get longer supersonic jet propagation into the molten metal, a supersonic coherent jet is suggested as one of the alternatives which are applicable to the electric furnace system. It has a flame around the conventional supersonic jet and thus the entrainment effect of the surrounding gas into the supersonic jet is reduced, leading to a longer propagation of the supersonic jet. In this regard, gasdynamics mechanism about why the combustion phenomenon surrounding the supersonic jet causes the jet core length to be longer is not yet clarified. The present study investigates the major characteristics of the supersonic coherent jet, compared with the conventional supersonic jet. A computational study is carried out to solve the compressible, axisymmetric Navier-Stokes equations. The computational results of the supersonic coherent jet are compared with the conventional supersonic jets.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2010년 춘계학술대회논문집
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• pp.534-541
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• 2010

A high-order accurate Euler flow solver based on a discontinuous Galerkin method has been developed for the numerical simulation of unsteady flows on unstructured meshes. A multi-level solution-adaptive mesh refinement/coarsening technique was adopted to enhance the resolution of numerical solutions efficiently by increasing mesh density in the high-gradient region. An acoustic wave scattering problem was investigated to assess the accuracy of the present discontinuous Galerkin solver, and a supersonic flow in a wind tunnel with a forward facing step was simulated by using the adaptive mesh refinement technique. It was shown that the present discontinuous Galerkin flow solver can capture unsteady flows including the propagation and scattering of the acoustic waves as well as the strong shock waves.

• 한국전산유체공학회지
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• 제14권1호
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• pp.53-61
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• 2009

The objective of this research is to design blade planform to reduce high speed impulsive(HSI) noise from a non-lifting helicopter rotor using CFD method and optimization techniques. As for the aero-acoustic analysis, CFD technique for aerodynamic analysis and Kirchhoff's method for the acoustic analysis were used. As for the optimization method, Kriging-based genetic algorithm(GA) model as a high-fidelity optimization method was chosen. Design variables and constraints are determined for arbitrary blade planform. The result shows that the optimized blade planform with high swept-back and taper ratio can reduce HSI noise by suppressing generation of the strong shock wave on blade surface and propagation of the noise to the farfield flow region.

• 한국레이저가공학회지
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• 제6권3호
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• pp.37-45
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• 2003

Pulsed laser ablation is important in a variety of engineering applications involving precise removal of materials in laser micromachining and laser treatment of bio-materials. Particularly, detailed numerical simulation of complex laser ablation phenomena in air, taking the interaction between ablation plume and air into account, is required for many practical applications. In this paper, high-power pulsed laser ablation under atmospheric pressure is studied with emphasis on the vaporization model, especially recondensation ratio over the Knudsen layer. Furthermore, parametric studies are carried out to analyze the effect of laser fluence and background pressure on surface ablation and the dynamics of ablation plume. In the numerical calculation, the temperature, pressure, density, and vaporization flux on a solid substrate are obtained by a heat-transfer computation code based on the enthalpy method. The plume dynamics is calculated considering the effect of mass diffusion into the ambient air and plasma shielding. To verify the computation results, experiments for measuring the propagation of a laser induced shock wave are conducted as well.

• 한국지열·수열에너지학회논문집
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• 제18권3호
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• pp.7-18
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• 2022

Secondary batteries used in electric vehicles have a potential risk of ignition and explosion. Various safety measures are being taken to prevent these risks. A numerical study was performed using a computational fluid dynamics code on the cases where pressure relief vents that can reduce the blast overpressures of batteries were installed in the through-compression test room, short-circuit drop test room, combustion test room, and immersion test room in facilities rleated to battery used in electric vehicles. This study was conducted using the weight of TNT equivalent to the energy release from the battery, where the the thermal runaway energy was set to 324,000 kJ for the capacity of the lithium-ion battery was 90 kWh and the state of charge (SOC) of the battery of 100%. The explosion energy of TNT (△H_TNT) generally has a range of 4,437 to 4,765 kJ/kg, and a value of 4,500 kJ/kg was thus used in this study. The dimensionless explosion efficiency coefficient was defined as 15% assuming the most unfavorable condition, and the TNT equivalent mass was calculated to be 11 kg. The internal explosion generated in a test room shows the very complex propagation behavior of blast waves. The shock wave generated after the explosion creates reflected shock waves on all inner surfaces. If the internally reflected shock waves are not effectively released to the outside, the overpressures inside are increased or maintained due to the continuous reflection and superposition from the inside for a long time. Blast simulations for internal explosion targeting four test rooms with pressure relief vents installed were herein conducted. It was found that that the maximum blast overpressure of 34.69 bar occurred on the rear wall of the immersion test room, and the smallest blast overpressure was calculated to be 3.58 bar on the side wall of the short-circuit drop test room.

• 한국전산유체공학회지
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• 제19권4호
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• pp.68-74
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• 2014

This computational study features the transient compressible and inviscid flow analysis on a metallic plasma discharge from the opposing composite electrodes which is subjected to pulsed electric power. The computations have been performed using the flux corrected transport algorithm on the axisymmetric two-dimensional domain of electrode gap and outer space along with the calculation of plasma compositions and thermophysical properties such as plasma electrical conductivity. The mass ablation from aluminum electrode surfaces are modeled with radiative flux from plasma column experiencing intense Joule heating. The computational results shows the highly ionized and highly under-expanded supersonic plasma discharge with strong shock structure of Mach disk and blast wave propagation, which is very similar to muzzle blast or axial plasma jet flows. Also, the geometrical effects of composite electrodes are investigated to compare the amount of mass ablation and penetration depth of plasma discharge.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
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• pp.407-408
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• 2006

Passenger safety is one of the most important considerations in the purchase of an automobile. A curtain-type air bag is increasingly adapted in deluxe cars for protecting passengers from the danger of side clash. Inflator housing is a main part of the curtain-type air bag system for supplying high-pressure gases to pump up the air bag-curtain. Although the inflator housing is fundamental in designing a curtain-type air bag system, flow information on the inflator housing is very limited. In this study, we measured instantaneous velocity fields of a high-speed flow ejecting from the inflator housing using a dynamic PIV system. From the velocity field data measured at a high frame-rate, we evaluated the variation of the mass flow rate with time. From the instantaneous velocity fields of flow ejecting from the airbag inflator housing in the initial stage, we can see a flow pattern of broken shock wave front and its downward propagation. The flow ejecting from the inflator housing was found to have large velocity fluctuations and the maximum velocity was about 700m/s. The velocity of high-speed flow was decreased rapidly and the duration of high-speed flow over 400m/s was maintained only to 30ms. After 100ms, there was no perceptible flow.

• 한국터널지하공간학회 논문집
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• 제5권4호
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• pp.337-348
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• 2003

밀장전한 암반 발파공에서 화약 폭발시 발생하는 고압의 폭굉압력 전파메카니즘을 충격파 이론을 적용하여 규명하고 전달된 발파압력 산정식을 유도하였다. 유도된 발파압력 산정식은 폭굉파속도, 단열지수, 화약밀도, Hugoniot 상수, 암반밀도의 함수였다. 에멀젼 화약과 서울 화강암의 특성시험을 시행하여 각 특성치의 확률분포를 정의하고 발파압력 산정식에 적용하여 발파압력의 확률분포를 산출하였다. 화약 특성치와 암반 특성치의 확률분포는 정규분포를 나타냈으며 따라서 발파압력의 확률분포도 정규분포로 추정되었다. 발파압력에 대한 매개변수분석을 시행한 결과 폭굉파속도가 발파압력에 가장 크게 영향을 미쳤다. 또한 이런 특성치의 불확실성이 발파압력의 불확실성에 미치는 영향을 분석하였다. 분석결과 암반특성치의 불확실성이 화약특성치보다 더 크게 영향을 미쳤다. 비록 매개변수분석에서 폭굉파속도가 발파압력에 가장 크게 영향을 미치는 요소이지만 암반특성치의 불확실성이 폭굉파속도의 불확실성보다 더 크기 때문에 발파압력은 후자보다 전자에 의해서 더 크게 영향을 받는다.