• Title/Summary/Keyword: 간극의 영향

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Numerical Study of the Supersonic Turbine Rotor Tip Variation Effect on the Turbine Performance (로터 팁 간극이 초음속 터빈 성능에 미치는 영향에 대한 전산해석 연구)

  • Park, Pyun-Goo;Jeong, Eun-Hwan;Kim, Jin-Han;Lee, Soo-Yong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.11a
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    • pp.382-386
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    • 2006
  • Three dimensional numerical analysis of the supersonic turbines with different rotor tip clearances was conducted to analyze the effect of the tip gap clearance variations on the turbine performance. The result showed that the turbine performance deteriorates and the tip leakage increases by the effect of the rotor tip clearance and the tip leakage affects turbine performance degradation dominantly.

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Consideration on Influence Factor in Predicting Undrained Shear Strength and Pore Pressure Coefficient Using Critical State Theory (한계상태이론을 이용한 비배수 전단강도 및 간극수압계수 예측시 영향인자에 관한 검토)

  • 김영수;김기영;문홍득
    • Journal of the Korean Geotechnical Society
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    • v.17 no.4
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    • pp.57-70
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    • 2001
  • 한계상태이론은 정규압밀 및 과압밀시료에 대한 비배수 전단강도와 간극수압계수에 관한 식을 제안하고 있는데, 이 식은 3가지 상수를 포함하고 있다. 한계상태상수(M), 한계상태 간격비(${\gamma}$), 한계상태 간극수압계수(Λ)가 바로 그것이며, 이러한 상수는 각 모델 및 구하는 방법에 따라 그 차이가 발생함으로서, 전단강도 및 간극수압계수의 예측시 적지 않은 영향을 미치게 된다. 본 논문에서는 재 성형된 이암풍화토를 이용하여 등방삼축압축시험을 정규압밀과 과압밀로 나누어 실시하고 그 결과를 분석하였으며 이를 토대로 각 모델 및 방법에 따른 상수를 도출하였다. 그리고 이러한 상수의 차이가 비배수 전단강도 및 간극수압계수의 예측에 미치는 영향을 살펴보았다. 시험결과 정규압밀시료의 경우 각 상수의 변화에 따른 비배수 전단강도 및 간극수압계수는 상당한 차이를 보였으며, 한계상태간격비와 Λ값을 강도비로부터 얻어진 값을 사용한 경우가 결과치에 가장 잘 근접함을 알 수 있었다. 과압밀시료의 경우 역시 이들 상수에 따라 전단강도의 변화폭이 크게 나타났으며 정규압밀과 마찬가지로 강도비에서부터 도출된 상수를 적요한 경우 실측치에 가장 근접하였다. 반면 간극수압계수의 예측시에는 상수에 따른 변화폭이 크지 않았으며, 특히 과압밀비가 증가할수록 각 상수에 대한 영향이 작게 나타났다.

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Machine Learning Framework for Predicting Voids in the Mineral Aggregation in Asphalt Mixtures (아스팔트 혼합물의 골재 간극률 예측을 위한 기계학습 프레임워크)

  • Hyemin Park;Ilho Na;Hyunhwan Kim;Bongjun Ji
    • Journal of the Korean Geosynthetics Society
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    • v.23 no.1
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    • pp.17-25
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    • 2024
  • The Voids in the Mineral Aggregate (VMA) within asphalt mixtures play a crucial role in defining the mixture's structural integrity, durability, and resistance to environmental factors. Accurate prediction and optimization of VMA are essential for enhancing the performance and longevity of asphalt pavements, particularly in varying climatic and environmental conditions. This study introduces a novel machine learning framework leveraging ensemble machine learning model for predicting VMA in asphalt mixtures. By analyzing a comprehensive set of variables, including aggregate size distribution, binder content, and compaction levels, our framework offers a more precise prediction of VMA than traditional single-model approaches. The use of advanced machine learning techniques not only surpasses the accuracy of conventional empirical methods but also significantly reduces the reliance on extensive laboratory testing. Our findings highlight the effectiveness of a data-driven approach in the field of asphalt mixture design, showcasing a path toward more efficient and sustainable pavement engineering practices. This research contributes to the advancement of predictive modeling in construction materials, offering valuable insights for the design and optimization of asphalt mixtures with optimal void characteristics.

Effect of Side Friction on Consolidation Test of Normally Consolidated Kaolinite Slurry (정규압밀된 연약점토의 압밀시험시 측면 마찰의 영향)

  • Lee, Jangguen;Fox, Patrick J.
    • Journal of the Korean GEO-environmental Society
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    • v.9 no.3
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    • pp.61-68
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    • 2008
  • Side friction is often neglected in the analysis of the results of a consolidation test when the specimen has a high ratio of diameter to height. As the height of a specimen increases, however, side friction becomes important. This paper presents an investigation of the effect of side friction on consolidation test results for normally consolidated kaolinite slurry. Consolidation tests were performed to obtain settlement, pore pressure, compressibility, and hydraulic conductivity of kaolinite slurry. The compressibility relationship is corrected for side friction using a modified form of Taylor (1942) analytical solution. Numerical simulations using the CS2 piecewise-linear model are compared with settlement and excess pore pressure measurements. Experimental results show improved agreement with a modified CS2 model in which the effect of side friction is considered. The numerical and experimental results indicate that the side friction is an important factor affecting the rate of consolidation as well as the compressibility relationship for the specimen.

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Experimental Investigation of Turbopump Turbine : Turbine Performance and Effect of Nozzle-Rotor Clearance (터보펌프 터빈의 성능 및 노즐-로터 간극의 영향에 대한 실험적 고찰)

  • Jeong Eun-Hwan;Kang Sang-Hun;Shin Dong-Yoon;Park Pyu-Goo;Kim Jin-Han
    • Journal of the Korean Society of Propulsion Engineers
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    • v.10 no.2
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    • pp.78-86
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    • 2006
  • This paper presents the performance test result of the 30-ton class turbopump turbine. Test has been conducted using high pressure cold air, The turbine overall performance has been measured for various pressure ratio and rotational speed settings. The nozzle-rotor clearance effect on turbine performance also has been tested for the four kinds of the nozzle-rotor clearance values. We found that turbine efficiency rated 51.1% at its design velocity ratio and pressure ratio of 13.5. We also found that turbine efficiency can be increased by 3.5% for approximately 1mm decrement of the nozzle-rotor clearance from its nominal value.

Study on the Performance of a Centrifugal Compressor Using Fluid-Structure Interaction Method (유체-구조 연성해석을 이용한 원심압축기 운전익단간극과 성능 예측)

  • Lee, Horim;Kim, Changhee;Yang, Jangsik;Son, Changmin;Hwang, Yoonjei;Jeong, Jinhee
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.40 no.6
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    • pp.357-363
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    • 2016
  • In this study, we perform a series of aero-thermo-mechanical analyses to predict the running-tip clearance and the effects of impeller deformation on the performance using a centrifugal compressor. During operation, the impeller deformation due to a combination of the centrifugal force, aerodynamic pressure and the thermal load results in a non-uniform tip clearance profile. For the prediction, we employ the one-way fluid-structure interaction (FSI) method using CFX 14.5 and ANSYS. The predicted running tip clearance shows a non-uniform profile over the entire flow passage. In particular, a significant reduction of the tip clearance height occurred at the leading and trailing edges of the impeller. Because of the reduction of the tip clearance, the tip leakage flow decreased by 19.4%. In addition, the polytrophic efficiency under operating conditions increased by 0.72%. These findings confirm that the prediction of the running tip clearance and its impact on compressor performance is an important area that requires further investigation.

Effect of a Gap of a 2-D Flap Rudder on the Lift (2차원 플랩타의 간극이 양력에 미치는 영향)

  • Chang-Gu Kang
    • Journal of the Society of Naval Architects of Korea
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    • v.30 no.4
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    • pp.31-38
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    • 1993
  • Horn rudders or flap rudders with a gap between forward and after part are used for effective steering of a ship or a submerged body. It is necessary to analyze the effect of a gap since it affects the performance of rudders. In this paper, an equation to calculate the lift acting on a two-dimensional flap rudder in uniform flow is derived by using the thin hydrofoil theory and the analytic solution of viscous flow in a channel formed by two coaxial cylindrical walls to which a pressure gradient is applied.

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Dynamic Characteristics of Gravity Quay Wall during Generation of Excess Pore Pressure in Backfill Soils (뒤채움지반에서의 과잉간극수압 발생이 중력식 안벽구조물의 동적특성에 미치는 영향 분석)

  • Hwang Jae-Ik;Kim Myoung-Mo
    • Journal of the Korean Geotechnical Society
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    • v.21 no.1
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    • pp.123-131
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    • 2005
  • In this research, shaking table tests for three types of gravity quay wall system were performed to analyze the influence of excess pore pressure in backfill soils on the natural frequency of gravity quay wall systems. The elastic modulus of backfill soils was also estimated from the back analyses using the results of the shaking table tests. From the test results, it was observed that as the magnitude of excess pore pressures increased, the natural frequency of the gravity quay wall system decreased and vice versa. The natural frequency was about 44Hz when no excess pore pressure was generated in backfill soils, and decreased to about 16Hz at the pore pressure ratio of 0.55. The elastic modulus of backfill soils reached the constant maximum value when the pore pressure ratio was less than 0.2, and abruptly decreased as the pore pressure ratio became larger than that. The elastic modulus of backfill soils decreased to $10\%$ of the maximum value when the pore pressure ratio was 0.55.

The Effects of Stress and Time History on Pore Pressure Parameter of Overconsoldated clay (과압밀점토의 간극수압계수에 응력이력과 시간이력이 미치는 영향)

  • 김수삼;김병일;한상재;신현영
    • Journal of Korean Society of Coastal and Ocean Engineers
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    • v.14 no.4
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    • pp.286-294
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    • 2002
  • This study investigated the effects of stress and time history of overconsolidated clayey soils on pore pressure parameter, A. Laboratory tests were carried out under the conditions of both varying stress and time history. The stress history is classified into (i) rotation angle of stress path, (ii) overconsolidation ratio, and (iii) magnitude of length of recent stress path. The time history is divided into (i) loading rate of recent stress path and (ii) rest time. Pore pressure parameters are different both in the magnitude and trend with the rotation angle, depending on the magnitude of overconsolidation ratio but not in a trend. In addition, the pore pressure parameters have no effects on the magnitude of length of recent stress path except the level of initially small strain, while loading rates of recent stress path have effects on it. Finally, the pore pressure parameters of overconsolidated clays increase with the existence of the rest time, until either the deviator stress exceeds 70 kPa or the strain up to 0.1%.

Numerical Investigation of the Effect of Nozzle-Rotor Axial Clearance on the Supersonic Turbine Performance (노즐-로터 간극이 초음속 터빈의 성능에 미치는 영향에 대한 수치해석 연구)

  • Park Pyun-Goo;Jeong Eun-Hwan;Kim Jin-Han
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.05a
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    • pp.331-336
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    • 2006
  • This paper studies the effects of the nozzle-rotor axial clearance of a supersonic turbine on turbine performance. The nozzle-rotor axial clearance of the supersonic turbine developed to drive a turbopump for 30 ton class liquid rocket engines was varied and a numerical analysis of the turbines having the different nozzle-rotor axial clearances was conducted. It has been found that turbine performance degrades with an increasing axial clearance due to the increased stagnation pressure loss in the axial clearance region.

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