• 한국해양공학회지
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• 제24권2호
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• pp.1-9
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• 2010

Oscillating Water Column is one of the most widely used converting systems all over the world. The operating performance is influenced by the efficiencies of the two converting stages in the OWC chamber-turbine integrated system. In order to study the effects of the pressure drop induced by the air turbine, the experiments using the impulse turbine and the orifice device are carried out in the wave simulator test rig. The numerical simulation utilizing the orifice and porous media modules is calculated and validated by the corresponding experimental data. The numerical wave tank based on the two-phase VOF model embedded with the above modules is employed to investigate the wave elevation, pressure variation inside the chamber and the air flow velocity in the duct. The effects of the air turbine on the integrated system and interaction among the wave elevation, pressure and air flow velocities variations are investigated, which demonstrates that the present numerical model are more accurate to be employed.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제35회 추계학술대회논문집
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• pp.717-722
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• 2010

초음속 풍동은 실험하고자 하는 모델 주위에 인공적으로 초음속 유동장을 형성하여 모델에 작용하는 현상을 관찰 및 측정하는 실험 장비이다. 이러한 풍동 실험 장비는 비행체 설계에 있어 시제기를 제작하지 않고도 비행체 외형에 대한 공기역학적 특성을 파악하는데 유용하다. 본 연구에서는 러시아에서 제작된 초음속/극초음속 풍동(MAF : The Model Aerodynamic Facility)을 시험 시간 증가 및 활용성 증가를 목적으로 개조하였다. 안전성 확보 및 원격 작동을 위해 공압 밸브를 설치, 실험 시간의 증가를 위해 새 저장 탱크를 설치했다. 설치한 밸브와 탱크를 이용할 수 있도록 배관 시스템을 개조하였다. 또한 광학적 시험을 위하여 시험부의 광학창을 확장하였다. 개조 후 마하수 2,3,4에 대하여 성능 시험을 수행하였다. 유동가시화 기법중 하나인 Shadow graph 기법을 이용하여 초음속 유동장의 형성을 확인하였으며, 마하수 2,3,4에 대하여 Settling Chamber, Working section의 압력측정을 통해 성능 시험을 수행하였다. 결과로부터 해당 초음속 풍동에 사용가능한 모델 크기 및 시험 시간을 도출하였다.

• 한국추진공학회지
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• 제12권1호
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• pp.7-15
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• 2008

Pressure Sensitive Paint(PSP)는 압력에 반응하는 도료를 뜻한다. PSP를 이용하여 압력을 측정하기 위해서는 Paint Calibration과 PSP를 도포한 모델의 풍동실험이 필요하다. PSP는 이 두 가지의 결과를 이용한 이미지의 후처리과정을 통하여 압력정보를 포함한 이미지를 얻을 수 있는 신기술이다. 본 연구에서는 PSP에 필요한 장치 및 설비들을 구성하고 PSP를 이용하여 초음속 유동장 내의 압력측정 실험을 실시하였다. 압력측정 실험은 초음속 유동장의 노즐 벽면의 압력을 측정하였으며, 측정 압력에 대해서는 압력공(Pressure Tap)에 의한 결과값과 전산해석의 결과값을 통하여 비교하였고, 그 실험 결과를 바탕으로 PSP는 표면압력을 측정함에 있어서 압력공을 이용한 기존의 방식을 대체할 수 있는 기술임을 확인하였다.

• 대한전기학회논문지:전기기기및에너지변환시스템부문B
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• 제53권12호
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• pp.725-731
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• 2004

In this study, the three type hybrid interrupters according to the arrangement of the thermal expansion chamber and the puffer cylinder(they are called 'serial type', 'parallel/exchanged type', and 'parallel/separated type' respectively in this work) were designed and manufactured. This paper presents the tested results of the thermal recovery characteristics on the interrupters using a simplified synthetic test facility. The 'serial type' hybrid interrupter which is to obtain more easily the pressure rise for the thermal recovery compared with the others has the best capability in the thermal recovery characteristics. In order to investigate the stress on the operating mechanism, the distortion of the stroke wave in on-load test was examined to the stroke curve in no-load test. The biggest distortion was occurred in the 'parallel/exchanged type' hybrid interrupter. Finally, the small interruption capability on the three type interrupters was estimated by a theoretical form and the 'parallel/separated type' hybrid interrupter has the advantage of the others in the view of structure.

• 한국자동차공학회논문집
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• 제9권4호
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• pp.18-26
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• 2001

OSKA engine was developed to remove the dense core of injection sprays. The engine uses impinging spray on a small pip, which spray after impinging is broken into smaller drops and disperses into fee space in chamber. In this paper the pip size is analyzed to give more dispersion of spray and fuel vapor. The gas phase is modelled by the Eulerian continuum conservation equations of mass, momentum, energy and fuel vapour fraction. The liquid phase is modelled following the discrete droplet model approach in Lagrangian form, and the droplet wall interaction is modelled as a function of the velocity normal to impaction lands. The droplet distributions, vapor fractions and gas flows are analyzed for various injection pressure cases. Numerical results indicate that the land diameter of 5.6mm has the best performance of spray dynamics and vaporization in the test sizes.

• Journal of Mechanical Science and Technology
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• 제20권2호
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• pp.286-294
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• 2006

Flows in a ramjet inlet is simulated for the study of the rocket-ramjet transition. The flow is unsteady, two-dimensional axisymmetric, compressible and turbulent. Double time marching method is used for the unsteady calculation and HLLC method is used as a higher order MUSCL method. As for turbulent calculation, $\kappa-\omega$ SST model is used for more accurate viscous calculations. Sinusoidal pressure perturbation is given at the exit and the flow fields at the inlet is studied. The cruise condition as well as the ground test condition are considered. The pressure level for the ground test condition is relatively low and the effect of the pressure perturbation at the combustion chamber is small. The normal shock at the cruise condition is very sensitive to the pressure perturbation and can be easily detached from the cowl when the exit pressure is relatively high. The sudden decrease in the mass flux is observed when the inlet flow becomes subcritical, which can make the inlet incapable. The amplitude of travelling pressure waves becomes larger as the downstream pressure increases, and the wavelength becomes shorter as Mach number increases. The phase difference of the travelling perturbed pressure wave in space is 180 degree.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집D
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• pp.846-851
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• 2001

For the successful development of the main engine of KSR(Korea Sounding Rocket)-III, Korea Aerospace Research Institute(KARI) carried out the experimental study on the subscale model engines. Several types of engines were tested on the Small Liquid Rocket Engine Test Facility. One of the typical test results of a Sub. engine(Sub. Mod.3) is presented here. It uses the Jet A-1 as fuel, liquid oxygen as oxidizer, and Tri-Ethyl Aluminium(TEA1) as ignition agent. The gas pressure feed system is adopted as a feeding mechanism and the design chamber pressure is 200psia. The physical phenomena are described in three regimes(ignition, transient, and steady state) with the pressure, thrust, flowrate and image data. And the pressure oscillation is analyzed in Fourier domain (<500Hz). Then we conclude that in this experiment, the engine shows the characteristic low frequency of 80Hz and it is stable for that frequency of pressure oscillation.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.442-447
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• 2008

A numerical analysis has been conducted to investigate and characterize the unsteadiness of flow structure and oscillatory vacuum pressure inside of a supersonic diffuser equipped to simulate the high-altitude rocket test on the ground. A physical model of concern includes a rocket motor, a vacuum chamber, and a diffuser, which have axisymmetric configurations, using nitrogen gas as a driving fluid. Emphasis is placed on investigating physical phenomena of very complex and oscillatory flow evolutions in the diffuser operating at very close to the starting condition, i.e. minimum starting condition, which is one of major important parameters in diffuser design points of view.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2006년도 제27회 추계학술대회논문집
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• pp.271-274
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• 2006

Polyethylene-GOX 추진제를 이용한 소형 하이브리드 로켓 모터의 성능 예측 모델에 대한 연구를 수행하였다. 제안된 모델에서 연소실 전체에 걸친 상태량을 단일 변수로 가정하여 내탄도 모델 식을 풀어 연소실 내 압력을 예측할 수 있었으며, 실험을 통해 측정된 값과 비교하여 모델의 정확도를 고찰하였다.

• 대한토목학회논문집
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• 제34권3호
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• pp.907-917
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• 2014

연약지반을 매립후 굴착을 시행할 경우 흙막이벽체를 설치하더라도 배면지반에 지반파괴가 발생한다. 이를 최소화하기 위해 억지말뚝을 적용 후 실내모형 실험을 시행하여 억지효과를 규명하였다. 모형토조내 점토를 충진하고 계측시스템을 이용하여, 무보강일 경우와 억지말뚝으로 보강한 경우를 설정하여 굴착에 따른 배면지반의 침하, 간극수압, 토압을 측정하였다. 모형실험 결과 억지말뚝으로 보강할 경우 무보강시와 비교할 때 굴착 단계의 증가와 배면지반의 침하가 감소된 것으로 평가되었다. 간극수압은 보강여부와는 크게 상관없었고, 침하율은 적게 나타났다. 또한, 굴착깊이가 배면지반에 매우 큰 영향을 미치고, 굴착지점과 가까울수록 최대 침하가 발생되는 것으로 평가되었다.