• 대한조선학회논문집
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• 제48권5호
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• pp.396-403
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• 2011

The concept of an air lubrication has long been an object of attention since it can be utilized to reduce the frictional resistance, and what is more, it is eco-friendly. The present study examines the basic characteristics of an air cavity with intention of applying the air lubrication technology to the reduction of the resistance of a ship without excessive power increment. For the purpose, an air cavity was created at the bottom of a flat plate by injecting air behind a backward step and the hydrodynamic properties of the air cavity and the surrounding flow has been investigated experimentally and numerically. The influence of the step height and the air flow rate have been more carefully studied since they are presumed to be the main parameters affecting the characteristics of an air cavity. The results indicates that the shapes of the air cavities attached on the flat plate become "U" or "V" type depending on the incoming flow velocity and air flow rate. The study also confirms that the length of the air cavity increases with increase in air flow rate but there is a certain critical limit in the flow rate above which increase in the air cavity length is no more evident.

• 한국연소학회지
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• 제12권2호
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• pp.20-25
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• 2007

The supersonic combustion experiments are carried out using T3 free-piston shock tunnel. Hydrogen Fuel is injected in the cavity parallel with air(or nitrogen) flow. The equivalence ratios in this study are 0.132 and 0.447. Experimental measurements use OH-PLIF near the cavity and pressures in the combustor. For parallel fuel injection case, direct fuel add into cavity leads to increase of cavity pressure. And Flame exists just near the bottom wall for low equivalent ratio. There is no flame in the cavity because of no mixing in it. Compared to the inclined fuel injection, ignition delay length is longer for low equivalence ratio in both case. OH distribution is not a single line but a repeatable fluctuation flame structure by turbulence. Pressure distributions have nothing to do with the fuel injection position.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2007년도 제34회 KOSCO SYMPOSIUM 논문집
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• pp.31-36
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• 2007

The supersonic combustion experiments are carried out using T3 free-piston shock tunnel. Hydrogen Fuel is injected in the cavity parallel with air(or nitrogen fuel) flow. The equivalence ratios in this study are 0.132 and 0.447. Experimental measurements use OH-PLIF near the cavity and pressures in the combustor. For parallel fuel injection case, direct fuel add into cavity leads to increase of cavity pressure. And Flame exists just near the bottom wall for low equivalent ratio. There is no flame in the cavity because of no mixing in it. Compared to the inclined fuel injection, ignition delay length is longer for low equivalence ratio in both case. OH distribution is not a single line but a repeatable fluctuation flame structure by turbulence. Pressure distributions have nothing to do with the fuel injection position.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년도 춘계학술대회논문집
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• pp.452-455
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• 2008

A new passive control technique of cavity-induced pressure oscillations has been investigated numerically for a supersonic two-dimensional flow over open rectangular cavities at Mach number 1.83 just upstream of a cavity, in which a sub-cavity system is installed on the backward-facing step of the main cavity. A third-order TVD (Total Variation Diminishing) finite difference scheme with MUSCL is used to discretize the spatial derivatives in the unsteady compressible Navier-Stokes equations. The results obtained show that the present sub-cavity system is very effective in reducing cavity-induced pressure oscillations. The results also showed that the resultant amount of attenuation of cavity-induced pressure oscillations was dependent on the length and thickness of the flat plate, and also on the depth of the sub-cavity used as an oscillation suppressor.

• 전자공학회논문지D
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• 제36D권3호
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• pp.75-84
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• 1999

주입전류가 문턱전류 이상일 때 선폭증가계수, 구속계수, 내부손실과 레이저의 길이가 λ/4 위상천이 DFB레이저의 단일모드 이득차와 발진주파수의 변화에 미치는 영향에 대하여 체계적으로 연구하였다. 구속계수나 선폭증가계수와 구속계수의 곱으로 주어지는 변수보다 선폭증가계수가 단일모드 이득차 및 발진주파수에 미치는 영향이 크다. 내부손실이나 레이저 길이 각각의 값보다 내부손실과 레이저 길이의 곱으로 정의되는 정규화된 내부손실이 DFB 레이저의 단일모드 이득차 및 발진주파수의 변화에 미치는 영향이 크다. 정규화된 내부손실이 같은 경우에는 내부손실계수보다 레이저의 길이가 동작특성에 미치는 영향이 큼을 알 수 있었다. 또한 양자우물 레이저가 builk 레이저에 비하여 선폭증가계수가 작기 때문에 구속계수와 정규화된 내부손실 값의 변화에 따른 단일모드 이득차의 감소와 발진주파수의 변화가 작음을 보았다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2005년도 추계 학술대회논문집
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• pp.245-248
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• 2005

SCRamjet is the key technology for hypersonic flight over mach number 6. It is characterized by very short residence time in combustor because its internal flow is supersonic. In this short time, the whole process of combustion must be done. Especially numerical study of combustor is important because air-fuel mixing rate influences the performance of combustor. Various methods of air-fuel mixing enhancement are proposed. Among these, cavity injection method is selected to study in this paper. The numerical study is conducted with the variation of the cavity length at the fixed height of unit and jet injection on the downstream of cavity.

• 한국대기환경학회지
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• 제10권2호
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• pp.116-123
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• 1994

The E- $\varepsilon$ turbulence numerical model was applied to a flow around triangular ridge in neutral boundary layer. Scale of cavity region, mean velocity, Reynolds stress and eddy diffusivity were investigated. The height of cavity region was in satifactory agreement with the wind tunnel data while the length of cavity region was underestimated. The man wind velocities outside the cavity region were well Predicted by the model, however in cavity region the mean wind velocities of wind tunnel data were larger than the model results Reynolds stress of cavity region was overestimated by the model. The eddy diffusivity of wake region was strongly modified under the influence of triangular ridge. The local minimum of the eddy diffusivity was occured in the lee of the ridge top.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2008년도 추계학술대회B
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• pp.2782-2787
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• 2008

The subcavity passive control technique is used in present study. Cavity-induced pressure oscillation has been investigated numerically for a supersonic three-dimensional flow over rectangular cavities at Mach number 1.83 at the cavity entrance. Time dependent supersonic turbulent flow over cavity were examined by using the three-dimensional, mass-averaged Navier-Stokes equations based on a finite volume scheme and large eddy simulation. The results showed that the resultant amount of attenuation of cavity-induced pressure oscillations was dependent on the length and thickness of the flat plate.

• Design & Manufacturing
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• 제17권4호
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• pp.57-62
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• 2023

As a representative method for mass production, a multi-cavity type mold capable of simultaneously molding products of the same shape can be applied. It has the advantage of improving the productivity from several times to several tens of times, but it may cause disadvantages which is the quality deviation with each cavity. This study, therefore, has tried to increase the cavity filling balance by using a melt flipper and a flow distance control part in the runner part of the mold. Along with this, the design and manufacturing of air vents during injection molding have been verified through experimental methods to achieve a higher level of multi-cavity filling balance and dimensional accuracy.

• 한국양식학회지
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• 제11권4호
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• pp.529-546
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• 1998

부화직후 1.9 mm였던 자어는 부화후 47일경 19 mm전후로 성장하며 초기성장기 자어류들의 전장과 체중과의 관계는 $BW=4.45{\times}10^{-6}TL^{3.4718}$, r=0.9820이었다. 해상가두리의 사육개체는 최대어 전장 28.4 cm까지 성장한 개체를 사용하였고 이들 개체의 전장과 체중과의 관계는 $BW=2.36{\times}10^{-2}TL^{2.9180}$, r=0.9971이었다. 미분화된 참돔의 생식소부위는 생식소와 지방체로 구성되어 있으며 분화가 진행되어 생식소가 비후됨에 따라 지방체는 점점 수축되어 갔다. 부화후 6개월의 미분화기까지 발달한 생식소부위는 생식소와 곤봉상의 지방체로 구성되었다. 이들 생식소는 미세한 반투명산으로 생식원세포를 구별할 수 없는 미발달생태를 유지하고 있다. 부화후 7개월부터 생식소 상피조직의 발달로 생식상피를 식별할 수 있었고, 부화후 8개월 생식소는 난원세포의 발달로 성분화가 시작되었다. 이후 9개월 생식소 내강상피 전체에 초기 난모세포들이 발달하고 이들 난모세포들의 증가로 생식소내강은 난소강을 이룬다. 부화후 13개월 난모세포는 생식소전체를 채우게 되고 곧 난모세포들의 세포질 붕괴가 시작된다. 15개월부터는 난소강을 중심으로 새로운 초기 난모세포들이 발달하여 난소조직으로 된다. 그리고 공포상조식은 정원세포들이 분열.증식하여 정소조직을 이루게 된다. 이후 이들은 생식소자웅동체기를 지나 암.수로 성이 결정된다. 따라서 참돔은 유시자웅동체 juvenile hermaphrodite 이고 미분화자웅이제 경골어류 undifferentiated gonochoristic teleost이었다. 생식소 자웅분화상은 미분화기, 유사난원세포기, 유사난소기, 난소발달기, 정소형자웅동체기, 난소형자웅동체기 및 정소발달기로 구분되었다. 미분화기 생식소는 부화후부터 13개월, 전장 18cm까지 지속되었으며, 유사난원세포기는 부화후 7~13개월, 전장 11~18cm까지 지속되었다. 유사난소기는 부화 10~14개월, 전장 14~26cm까지이며, 난소발달기는 부화후 14개월, 전장 20cm부터 시작되었다. 부화후 20개월에는 전 조사개체의 44%가 난소였다. 난소형자웅동체기는 부화후 15개월, 전장 19~20cm부터 출현하며, 부화후 20개월, 전장 28~29cm에서는 관찰되지 않았다. 정소형자웅동체는 부화후 15개월, 전장 21~22cm에서 첫 출현한 후 20개월까지 지속되었다. 정소발달기는 부화후 15개월, 전장 21~22cm에서 첫 출현한 후 20개월의 39%, 전장 28~29cm의 33%를 차지하였다. 50%이상의 성분화발현은 부화후 11개월, 전장 16cm부터였다. 성결정은 암컷이 부화후 14개월, 전장은 20mc, 수컷이 부화후 15개월, 전장 20cm에 시작되었다. 50%이상의 성결정은 부화후 17개월, 전장 23cm에 일어났다