• 터널과지하공간
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• 제30권3호
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• pp.242-255
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• 2020

본 연구에서는 FLAC3D가 Opalinus Clay 암반의 열-수리-역학적 복합거동을 재현하고 이를 예측할 수 있는지 그 적용성을 검토하고자 국제공동연구 DECOVALEX-2015에서 참여하였으며, 그 일환으로 스위스 Mont Terri Rock Laboratory에서 수행된 Heater Experiment-D (HE-D)에 대한 모델링을 수행하였다. FLAC3D를 이용한 수치해석의 타당성을 평가하기 위해 현장시험에서 계측된 16 지점의 온도, 6 지점의 공극수압, 그리고 22 지점의 변형률 데이터와 비교하였다. 대상 암반의 열-수리-역학적인 이방성을 고려함으로써 Opalinus Clay 암반의 온도 변화 그리고 온도변화에 따른 공극수압의 변화와 같은 열-수리적 거동은 전반적으로 유사하게 나타났으나, 역학적 거동의 경우 변형률 데이터를 비교했을 때 온도와 공극수압과는 달리 계산된 변형률 일부만이 유사한 거동을 보였다.

• 터널과지하공간
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• 제30권3호
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• pp.193-213
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• 2020

사용후핵연료 심층처분장 처분공에 설치된 압축 벤토나이트 완충재가 처분공 내벽에 형성된 굴착손상영역 불연속면 내로 침투하는 현상을 보다 더 현실적으로 모사할 수 있는 수학적 모델이 개발되었다. 이 모델에서는 압축 벤토나이트의 침투를 평행 평판 암반 절리을 통한 Bingham 유체의 이동으로 가정한다. 개발된 모델에 의해 벤토나이트의 침투현상을 분석한 결과, 암반 절리를 통해 압축 벤토나이트가 침투하는 최대 깊이는 포화 압축 벤토나이트의 팽윤압과 암반 절리의 폭에 비례하며, 압축 벤토나이트의 항복강도에 반비례하였다. 압축 벤토나이트의 점도는 압축 벤토나이트의 침투 속도를 좌우하나, 최대 침투깊이에는 영향을 미치지 않는다.

• 터널과지하공간
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• 제30권4호
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• pp.335-358
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• 2020

본 연구에서는 TOUGH-FLAC 연동해석기법을 통해 단층의 수리역학적 거동을 평가할 수 있는 수치해석 모델을 제안하였다. 이는 국제공동연구 DECOVALEX-2019 Task B의 일환으로 수행되었으며, 불투수성 암반 내 유체 주입으로 인한 단층의 재활성을 예측하고 주변 암반의 수리역학적 안정성을 평가할 수 있는 해석모델을 개발하는 데에 그 목적이 있다. 본 연구에서는 TOUGH2 수리유동모델과 FLAC3D의 역학적 인터페이스 모델의 연동을 통해 단층의 역학적 거동을 보다 합리적으로 구현할 수 있는 해석기법을 제안하고, 벤치마크 해석과 스위스 Mont Terri 지하연구시설 현장시험에 적용하여 그 타당성과 유효성을 검증하였다. 개발된 해석 모델은 유체의 주입으로 인한 단층 내 압력 분포의 발달, 역학적 변형에 따른 수리간극의 변화, 변위와 응력 등 단층의 수리역학적 거동을 적절히 재현할 수 있는 것으로 나타났다.

• International Journal of Aeronautical and Space Sciences
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• 제16권4호
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• pp.493-499
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• 2015

The aerodynamic performance of blunt trailing edge airfoils was investigated. The flow fields around the modified NACA64-418, which consists of the tip blade of the wind turbine and Mexico model of IEA wind, were analyzed. To imitate the repaired airfoil, the original NACA64-418 airfoil, a cambered airfoil, is modified by the adding thickness method, which is accomplished by adding the thickness symmetrically to both sides of the camber line. The thickness ratio of the blunt trailing edge of the modified airfoil, $t_{TE}/t_{max}$, is newly defined to analyze the effects of the blunt trailing edge. The shape functions describing the upper and lower surfaces of the modified NACA64-418 with blunt trailing edge are obtained from the curve fitting of the least square method. To verify the accuracy of the present numerical analysis, the results are first compared with the experimental data of NACA64-418 with high Reynolds number, $Re=6{\times}10^6$, measured in the Langley low-turbulence pressure tunnel. Then, the aerodynamic performance of the modified NACA64-418 is analyzed. The numerical results show that the drag increases, but the lift increases insignificantly, as the trailing edge of the airfoil is thickened. Re-circulation bubbles also develop and increase gradually in size as the thickness ratio of the trailing edge is increased. These re-circulations result in an increase in the drag of the airfoil. The pressure distributions around the modified NACA64-418 are similar, regardless of the thickness ratio of the blunt trailing edge.

• 지질공학
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• 제17권3호
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• pp.367-379
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• 2007

본 연구에서는 부산광역시 도심지역인 부산진구 양정동에서 동구 수정동까지의 주로 경부고속철도 터널 통과 예정지역 지반조사로부터 얻어진 시추공 자료, 지하수위 자료, 공내 유향 유속 자료 그리고 현장수리시험 분석 자료를 바탕으로 천부지층과 수리지질 특성의 관련성을 평가하였다. 지하수위(Y)와 지형고도(X)의 관계식은 Y=0.75X-7.00 이며, 상관계수는 0.75로서 비교적 높은 편이다. 매립층, 충적층, 풍화대의 두께와 지하수위의 상관성을 살펴본 결과, 풍화대의 두께(A)의 자연로그값과 지하수위(Y)의 상관성이 상대적으로 높게 나타났으며, 그 회귀식은 Y=exp(9.974A)-14.155과 같다. 지하수 유향 유속 결과, 지하수 유향은 대체적으로 남쪽-남서쪽으로 향하고 있으며, 이는 지역적인 지하수위 분포와 대체로 일치한다.

• 한국지반환경공학회 논문집
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• 제7권6호
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• pp.133-143
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• 2006

본 논문에서는 저자가 제안한 유효응력모델을 이용하여 지진시 사면의 동적거동에 관한 수치해석을 수행하였다. 항복함수는 동일한 응력비를 가진 무한개의 방사선을 의미하며, 비관련 유동규칙을 가진 탄소성모델인 UBCSAND를 이용하였다. 이 모델은 FLAC내에 내장된 Mohr-Coulomb모델을 변형한 형태이다. UBCSAND모델을 이용하여 RPI에서 수행한 원심모형실험결과를 예측하였다. 먼저, UBCSAND모델을 Nevada모래를 사용한 반복 직접단순전단시험결과를 이용하여 검증하였으며, 액상화전후의 거동을 예측하였다. 이와 같이 검증된 모델을 원심모형실험에서 계측된 가속도, 과잉간극 수압, 변위와 서로 비교하였다. 일반적으로 계측치와 예측치가 일치하였다. 유효응력모델을 이용한 동적 수치해석기법은 서부 캐나다에서 댐, 교량, 터널, 파이프라인과 관련된 액상화 프로젝트에 실제 사용되고 있다.

• International Journal of Fluid Machinery and Systems
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• 제8권4호
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• pp.264-273
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• 2015

This presentation describes an experimental approach for the detection of cavitation in hydraulic machines by use of ultrasonic signal analysis. Instead of using the high frequency pulses (typically 1MHz) only for transit time measurement different other signal characteristics are extracted from the individual signals and its correlation function with reference signals in order to gain knowledge of the water conditions. As the pulse repetition rate is high (typically 100Hz), statistical parameters can be extracted of the signals. The idea is to find patterns in the parameters by a classifier that can distinguish between the different water states. This classification scheme has been applied to different cavitation sections: a sphere in a water flow in circular tube at the HSLU in Lucerne, a NACA profile in a cavitation tunnel and two Francis model test turbines all at LMH in Lausanne. From the signal raw data several statistical parameters in the time and frequency domain as well as from the correlation function with reference signals have been determined. As classifiers two methods were used: neural feed forward networks and decision trees. For both classification methods realizations with lowest complexity as possible are of special interest. It is shown that two to three signal characteristics, two from the signal itself and one from the correlation function are in many cases sufficient for the detection capability. The final goal is to combine these results with operating point, vibration, acoustic emission and dynamic pressure information such that a distinction between dangerous and not dangerous cavitation is possible.

• Selected Papers of The Society of Naval Architects of Korea
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• 제1권1호
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• pp.76-90
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• 1993

A new propeller series is developed using the newly developed blade section (KH 18 section) which has better cavitation characteristics and higher lift-drag ratio at wade angle-of-attack range than a conventional section. The radial patch distribution of the new series propellers is variable stance they were designed adaptively to a typical wake distribution. Basic geometric particulars of the series propellers. such as chord length, thickness, skew and rake distributions, are determined on the basis of recent full scale propeller geometric data. The series is developed for propellers having 4 blades, and blade area ratios of 0.3, 0.45, 0.6 and 0.75. Mean pitch ratios are varied as 0.5, 0.6, 0.7, 0.95 and 1.1 for each blade area ratio. The new propeller series consists of 20 propellers and is named as the KD(KRISO-DAEWOO)-propeller series. Propeller open-water tests are performed at the towing tank, and cavitation observation tests and fluctuating pressure tests are carried out at the cavitation tunnel of KRISO. $B_{p}-\delta$ curves, which can be used to select the optimum propeller diameter at the preliminary design stage, are derived from a regression analysis of the propeller open-water test results. The KD-cavitation chart is derived from the cavitation observation test results by choosing the local maximum lift coefficient and the local cavitation number as parameters. The cavity extent predicted by the KD-cavitation chart would be more accurate compared to that by an existing cavitation charts, such as the Burrll's cavitation chart, since the former is derived from the cavitation observation test results in a typical ship's wake, while the lather is derived from the test results in a uniform flow.

• 대한조선학회논문집
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• 제42권6호
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• pp.619-630
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• 2005

A two-frame PIV (Particle Image Velocimetry) technique is used to investigate the wake characteristics behind a marine propeller with 4 blades at high Reynolds number. For each of 9 different blade phases from $ 0^{\circ} $ to $ 80^{\circ} $, one hundred and fifty instantaneous velocity fields are measured. They are ensemble averaged to study the spatial evolution of the propeller wake in the region ranging from the trailing edge to one propeller diameter (D) downstream location. The phase-averaged mean velocity shows that the trailing vorticity is related to radial velocity jump, and the viscous wake is affected by boundary layers developed on the blade surfaces and centrifugal force. Both Galilean decomposition method and vortex identification method using swirling strength calculation are very useful for the study of vortex behaviors En the propeller wake legion. The slipstream contraction occurs in the near-wake region up to about X/D : 0.53 downstream. Thereafter, unstable oscillation occurs because of the reduction of interaction between the tip vortex and the wake sheet behind the maximum contraction point.

• Wind and Structures
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• 제25권3호
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• pp.233-259
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• 2017

Investigations on simulated near-surface atmospheric boundary layer (ABL) in an open-jet facility are carried out by conducting experimental tests on small-scale models of low-rise buildings. The objectives of the current study are: (1) to determine the optimal location of test buildings from the exit of the open-jet facility, and (2) to investigate the scale effect on the aerodynamic pressure characteristics. Based on the results, the newly built open-jet facility is well capable of producing mean wind speed and turbulence profiles representing open-terrain conditions. The results show that the proximity of the test model to the open-jet governs the length of the separation bubble as well as the peak roof pressures. However, test models placed at a horizontal distance of 2.5H (H is height of the wind field) from the exit of the open-jet, with a width that is half the width of the wind field and a length of 1H, have consistent mean and peak pressure coefficients when compared with available results from wind tunnel testing. In addition, testing models with as large as 16% blockage ratio is feasible within the open-jet facility. This reveals the importance of open-jet facilities as a robust tool to alleviate the scale restrictions involved in physical investigations of flow pattern around civil engineering structures. The results and findings of this study are useful for putting forward recommendations and guidelines for testing protocols at open-jet facilities, eventually helping the progress of enhanced standard provisions on the design of low-rise buildings for wind.