• KSCE Journal of Civil and Environmental Engineering Research
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• v.13 no.5
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• pp.261-273
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• 1993

In order to study hydraulic properties and mechanical properties on unsaturated region, soil-water retention curve was obtained for suction plate method and pressure plate method, respectively. To investigate permeability of unsaturated soil and soil-water retention curve at the same time, unsaturated permeability tests using an improved Richard's method were performed on Joomoonjin Sand. These experimental results were compared with those by empirical equations. The relationship between air entry value and saturated permeability of filter was obtained for selecting a proper filter in unsaturated soil tests.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.30 no.11 s.254
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• pp.1057-1065
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• 2006

In order to figure out the physical meaning of 3-D angular flow index for in-cylinder bulk motion, CFD analysis for the swirl and tumble steady flow test rig were made using commercial package STAR-CD. Computer simulations and rig tests on some kinds of induced flow conditions were carried out. Finally, based on the comparison between the simulated results and measured results, the physical meaning of 3-D angular flow index $|\longrightarrow_{N_B}|$, $\beta$ composed of swirl and tumble coefficients measured by steady flow test rig was described.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.30 no.11 s.254
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• pp.1066-1073
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• 2006

Recently, because the variable induction systems are adopted to intake system, in-cylinder flow induced by induction system is very complex. Therefore it is very difficult to describe the in-cylinder bulk flow characteristics using the conventional swirl or tumble coefficient. In this study, in order to clarify the 3-D angular flow characteristics of in-cylinder bulk motion in the developing process of variable induction system, we introduced the new 3-D angular flow index, angular flow coefficient($N_B$) Finally, to confirm the index, we carried out the steady flow rig test for intake port of test engine varying valve lift on the test matrix.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.28 no.1
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• pp.1-8
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• 2004

An study has been performed with axisymmetric coflow diffusion flames to investigate the influence of air-side fuel side dilution and initial preheated temperature on the soot formation in methan/air flames. Soot quantities are determined by using PLII(Planar Laser Induced Incandescence), such a $C_2$H$_2$ major species(CH$_4$, $O_2$, $N_2$) and temperature are simulated by chemkin code. The numerical analysis was performed with transport properties and detailed reaction mechanisms m axisymmetric coflow diffusion flames. The study of how flame temperature and $N_2$ dilution of air and fuel side influence the soot concentrations is focused. Soot concentrations results on PLII show that preheated temperature contributes to an increase in the soot volume fraction, and soot formation Is more productive to air side dilution than to fuel side dilution. $C_2$H$_2$ concentrations have a similar tendency to soot concentrations.

• Transactions of the Korean Society of Mechanical Engineers
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• v.14 no.6
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• pp.1669-1678
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• 1990

The annular and coaxial swirl flows between which LPG is supplied was selected to study the swirling flames in double co-swirl flows. The objective of this study is to research into the effects of double co-swirl flow conditions on the stability limit, the reverse flow boundary, and the time mean temperature distributions of the swirling flames. The increase of swirl intensity of axial flow makes the stability limit decrease, but the annular swirl flow (SM>0.5) makes stability and swirl intensity of axial flow increase, And the existence of axial swirl flow makes flame intensive and small in size, and this may be applicable to the design of high power compact combustor.

• Proceedings of the Korean Vacuum Society Conference
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• 2014.02a
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• pp.312.2-312.2
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• 2014

실리콘은 광센서, 태양전지, 발광다이오드 등 광소자 응용 분야에서 널리 사용되고 있는 물질이다. 그러나 실리콘의 높은 굴절율(n~3.5)은 표면에서 약 30% 이상의 Fresnel 반사를 발생시켜 소자의 효율을 감소시키는 원인이 된다. 따라서, 반사손실을 줄이기 위해서는 실리콘 표면에 효율적인 무반사 코팅을 필요로 한다. 기존의 단일 혹은 다중 박막을 이용한 무반사 코팅 기술은 물질간 열팽창계수의 불일치, 접착력 문제, 박막 두께 조절 및 적합한 굴절율을 갖는 물질 선택 어려움 등의 단점을 지니고 있다. 최근, 이러한 무반사 코팅 기술의 대안으로 곤충 눈 구조를 모방한 나노크기의 서브파장 격자구조 (subwavelength gratings, SWGs)에 대한 연구가 활발히 이루어지고 있다. 이러한 SWGs 구조는 공기와 반도체 표면 사이에 점진적, 선형적으로 변화하는 유효굴절율을 갖기 때문에, 광대역 파장영역뿐만 아니라 다양한 각도에서 입사하는 빛에 대해서도 효과적으로 Fresnel 표면 반사를 낮출 수 있다. 본 연구에서는 실리콘 기판 표면 위에 효율적인 무반사 특성을 갖는 계층적 SWGs 나노구조를 제작하기 위해, 레이저간섭리소그라피 및 열적응집금속 입자를 이용한 식각 마스크 패터닝 방법과 유도결합플라즈마 식각 공정을 이용하였다. 제작된 무반사 실리콘 SWGs 나노구조의 표면 및 식각 프로파일은 전자주사현미경으로 관찰하였고, 표면 접촉각 측정 장비를 이용하여 샘플 표면의 젖음성을 확인하였다. 제작된 샘플의 광학적 특성을 조사하기 위해 UV-vis-NIR 스펙트로미터와 엘립소미터 측정 시스템들을 이용하였다.

• Membrane Journal
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• v.24 no.3
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• pp.240-248
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• 2014

Porous PVDF hollow fiber membranes were prepared by hybrid process of TIPS(thermally induced phase separation) and stretching for membrane distillation. The tests were conducted to investigate that permeability of the membrane could be enhanced by reducing membrane wall thickness. During fiber spinning, dope discharge rate from nozzle was reduced and flow rate of bore fluid increased to make the wall thickness thinner. As dope discharge rate from nozzle was reduced and flow rate of bore fluid increased, the membrane wall thickness was reduced. As a result, air permeability, water permeability and vapor permeability of the membranes increased.

• Proceedings of the KIEE Conference
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• 2002.07c
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• pp.1470-1472
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• 2002

3원계 51wt%Ni-4lwt%Cr-8wt%Si 합금 타겟을 가지고 DC/RF 마그네트론 스퍼터를 이용하여 박막저항을 제조하였고, 낮은 저항온도계수(TCR)를 가지는 박막을 만들기 위해 제조공정의 변화에 따른 박막의 미세구조와 전기적인 특성을 조사하였다. 스퍼터링 제조공정 변수로써 DC/RF Power, 반응압력, 기판온도를 변화시켰고, 제조된 박막은 공기중에서 $400[^{\circ}C]$까지 열처리 하였다. 반응압력을 감소시킴에 따라 TCR값은 감소하였고, 기판온도 및 열처리 온도의 증가에 따라 TCR값도 증가하였다. 또한, 비저항은 DC Power에서 $172[{\mu}{\Omega}cm]$, RF인 경우에는 $209[{\mu}{\Omega}cm]$을 나타내었고, 각각 +52, $-25[ppm/^{\circ}C]$의 TCR값을 나타냈다. 이와 같은 결과로부터 제조공정을 변화시킴에 따라 면저항 및 저항온도계수의 제어가 가능함을 알 수 있었다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.3
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• pp.1-5
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• 2006

Birds and insect in nature morph their mean camberline shapes to obtain both lift and thrust simultaneously. Previous unsteady thin airfoil theories were derived mainly for a rigid flapping airfoil. An extended unsteady thin airfoil theory for a deformable airfoil is required to analyze the unsteady two-dimensional aerodynamic characteristics of a biomorphing wing. Theodorsen's approach is extended to calculate the unsteady aerodynamic characteristics of a biomorphing airfoil. The mean camberline of the airfoil is represented as a polynomial. The unsteady aerodynamic characteristics of the morphing airfoil are represented as noncirculatory and circulatory terms. Present theory can be applied to the unsteady aerodynamic analysis of a flapping biomorphing airfoil and the aeroelastic analysis of a morphing wing.

• Journal of the Korean Magnetics Society
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• v.7 no.4
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• pp.180-185
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• 1997

Variations of core loss and coercivity with heat treatment condition have been studied in amorphous ribbon core specimens. All measurements were performed at 10 kHz with a maximum induction of 0.1 T. With increasing annealing time, both core loss and coercivity of core specimens decreased first, reaching minimum values, and increased thereafter. Specimen heat treated in an air showed better soft magnetic properties than those treated in Ar atmosphere. The specimens annealed under magnetic field higher than 6 Oe in radial direction showed reduced core loss and coercivity. The field annealing effects were increased with increasing cooling rate near Curie temperature of the material. The specimen annealed under an applied field in perpendicular direction of the core showed increased coercivity and decreased permeability.