• Wind and Structures
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• 제32권3호
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• pp.205-217
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• 2021

Cold regions with high air density and wind speed attract wind energy producers across the globe exhibiting its potential for wind exploitation. However, exposure of wind turbine blades to such cold conditions bring about devastating impacts like aerodynamic degradation, production loss and blade failures etc. A series of wind tunnel tests were performed to investigate the effect of icing on the aerodynamic properties of wind turbine blades. A baseline clean wing configuration along with four different ice accretion geometries were considered in this study. Aerodynamic force coefficients were obtained from the surface pressure measurements made over the test model using MPS4264 Simultaneous pressure scanner. 3D printed Ice templates featuring different ice geometries based on Icing Research Tunnel data is utilized. Aerodynamic characteristics of both the clean wing configuration and Ice accreted geometries were analysed over a wide range of angles of attack (α) ranging from 0° to 24° with an increment of 3° for three different Reynolds number in the order of 105. Results show a decrease in aerodynamic characteristics of the iced aerofoil when compared against the baseline clean wing configuration. The key flow field features such as point of separation, reattachment and formation of Laminar Separation Bubble (LSB) for different icing geometries and its influence on the aerodynamic characteristics are addressed. Additionally, attempts were made to understand the influence of Reynolds number on the iced-aerofoil aerodynamics.

• 한국항공우주학회지
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• 제34권10호
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• pp.1-6
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• 2006

본 연구에서는 3차원 날개의 실속 특성을 예측하였다. 날개의 실속 특성을 해석하기 위해 반복적 캠버변형 기법을 비평면 양력면 이론에 도입하였다. 반복적 캠버변형 기법은 기지의 2차원 에어포일 데이터를 이용하여 3차원 날개의 실속 특성을 해석한다. 날개의 한 단면에서의 캠버변형이 날개의 다른 단면에 미치는 영향은 다차원 뉴턴 반복법을 사용하여 고려하였다. 해석 결과는 실험값과 타 전산해석 결과와 비교하여 일치되는 결과를 보였다. 본 기법은 비틀림 또는 조종면을 갖는 어떠한 날개에도 적용이 가능하며 또한 날개와 날개의 상호 작용이 있을 때의 실속 특성도 예측 가능하다.

• 설비공학논문집
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• 제15권1호
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• pp.73-85
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• 2003

Four different methods of reducing the heat transfer coefficients from experimental data under dehumidifying conditions are compared. The four methods consist of two different heat and mass transfer models and two different fin efficiency models. Data are obtained from two heat exchanger samples having plain fins or wave fins. Comparison of the data with the reduction methods revealed that the single potential heat and mass transfer model yielded the humidity independent heat transfer coefficients. Two different fin efficiency models - enthalpy model and humidity model - yielded approximately the same fin efficiencies and accordingly approximately the same heat transfer coefficients. The heat transfer coefficients under wet conditions were approximately the same as those of the dry conditions for the plain fin configuration. For the wave fin configuration, however, wet surface heat transfer coefficients were approximately 12% higher. The pressure drops of the wet surface were 10% to 45% larger than those of the dry surface.

• 한국윤활학회:학술대회논문집
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• 한국윤활학회 1999년도 제29회 춘계학술대회
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• pp.317-324
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• 1999

The present work is an attempt to calculate the steady state pressure and perturbed pressure of herringbone grooved journal bearings. A generalized coordinate system is introduced to handle the complex bearing geometry. The coordinates are fitted to the groove boundary and the Reynold's equation is transformed to be fitted to this coordinates system using the Gauss divergence theorem. This method makes it possible to deal with an arbitrary configuration of a lubricated surface. The characteristics of finite herringbone grooved journal are well calculated using this method.

• Tribology and Lubricants
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• 제16권6호
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• pp.432-439
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• 2000

The present work is an attempt to calculate the steady state pressure and perturbed pressure of herringbone grooved journal bearings. A generalized coordinate system is introduced to handle the complex bearing geometry. The coordinates are fitted to the groove boundary and the Reynold's equation is transformed to be fitted to this coordinate system using the Gauss divergence theorem. This method makes it possible to deal with an arbitrary configuration of a lubricated surface. The caharacteristics of finite herringbone groove journal bearing are well calculated using this method.

• Tribology and Lubricants
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• 제7권2호
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• pp.41-45
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• 1991

An experimental investigation for leakage performance of five anti-swirl self-injection seals was carried out to select an optimum configuration for minimum leakage. Test results show that the self-injection mechanism with a plain seal generally degrades the leakage performance of noncontacting seals; however, through a series of the test program, an optimum anti-swirl self injection seal was selected to obtain a comparable leakage performance with a damper seal. A 12 holes anti-swirl and anti-leakage self-injected. configuration with a labyrinth surface gives minimum leakage among the tested anti-swirl self-injection seals.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 1996년도 추계학술대회 논문집
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• pp.567-571
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• 1996

The objective of STEP is to provide neutral mechanism capable of describing product data through the life cycle of a product, independent form any particular systems. This paper describes an STEP application program that can display the three-dimensional shape based on b-spline surface and the data which defines configuration of the product. The developed program is based on the STEP part 203 “Configuration controlled design”.

• 한국구조물진단유지관리공학회 논문집
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• 제19권3호
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• pp.104-112
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• 2015

본 논문에서는 비접촉 표면파 측정을 이용하여 콘크리트 슬래브에 발생한 표면균열의 깊이를 측정하기 위한 비파괴 검사법을 연구하였다. 이를 위하여 표면파 측정, 해석 및 균열 깊이 평가의 과정을 포함한 새로운 측정모델을 제안하였다. 먼저, 3차원 유한요소해석 모델을 이용하여 표면파의 에너지와 콘크리트 균열의 깊이의 상관관계를 표현하는 표면파 전달함수를 구하였다. 제안된 측정모델은 실험을 통하여 증명하였다. 한 쌍의 비접촉 센서를 이용하여 깊이 0~100mm의 10개의 표면균열을 포함한 콘크리트 슬래브 ($1500{\times}1500{\times}180mm^3$)을 통과하여 전달되는 표면파를 측정하였다. 측정모델은 콘크리트 균열 깊이에 대하여 약 최대 10%의 오차를 보이며 실제 깊이를 예측하는 것으로 나타났다. 비접촉 표면파 측정을 통하여 얻은 결과는 기존의 TOFD에 바탕을 둔 초음파법에서 얻은 결과보다 향상된 정확도를 보이는 것으로 나타났다. 특히 비접촉 센서의 특성상 매우 향상된 측정 속도 및 측정값의 일관성을 얻을 수 있었다. 본 연구에서는 모델의 실제구조물에 적용성에 관한 토의를 포함하고 있다.

• Journal of Mechanical Science and Technology
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• 제17권6호
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• pp.914-924
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• 2003

The interaction and breakdown of vortices over the Leading Edge Extension (LEX) - Delta wing configuration has been investigated through wing-surface pressure measurements, the off-surface flow visualization, and 5-hole probe measurements of the wing wake section. The description focused on analyzing the interaction and the breakdown of vortices depending on the angle of attack and the sideslip angle. The Effect of angle of attack and sideslip angle on the aerodynamic load characteristics of the model is also presented. The sideslip angle was found to be a very influential parameter of the vortex flow over the LEX-delta wing configuration. The introduction of LEX vortex stabilized the vortex flow, and delayed the vortex breakdown up to a higher angle of attack. The vortex interaction and breakdown was promoted on the windward side, whereas it was suppressed on the leeward side.

• 한국자동차공학회논문집
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• 제11권6호
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• pp.65-72
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• 2003

In order to clarify turbulent combustion characteristics of hydrocarbon mixtures by hydrogen addition, turbulent burning velocities in a constant volume vessel were measured for both lean and rich hydrocarbon mixtures. Moreover, the configuration characteristics of turbulent flame was investigated in the wrinkled laminar flame region. A laser tomography technique was used to obtain the images of turbulent flame, and quantitative analyses were performed. As a result, the characteristics of turbulent burning velocity was shown a distinct difference with the addition rate of hydrogen between lean and rich mixtures. On the other hand, the obtained tomograms showed that the surface area of turbulent flame depends almost only on the turbulence intensity.