• International Journal of Aeronautical and Space Sciences
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• 제16권2호
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• pp.190-205
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• 2015

In this paper, the impact damage behavior of USN-150B carbon/epoxy composite laminates subjected to high velocity impact was studied experimentally and numerically. Square composite laminates stacked with $[45/0/-45/90]_{ns}$ quasi-symmetric and $[0/90]_{ns}$ cross-ply stacking sequences and a conical shape projectile with steel core, copper skin and lead filler were considered. First high-velocity impact tests were conducted under various test conditions. Three tests were repeated under the same impact condition. Projectile velocity before and after penetration were measured by infrared ray sensors and magnetic sensors. High-speed camera shots and C-Scan images were also taken to measure the projectile velocities and to obtain the information on the damage shapes of the projectile and the laminate specimens. Next, the numerical simulation was performed using explicit finite element code LS-DYNA. Both the projectile and the composite laminate were modeled using three-dimensional solid elements. Residual velocity history of the impact projectile and the failure shape and extents of the laminates were predicted and systematically examined. The results of this study can provide the understanding on the penetration process of laminated composites during ballistic impact, as well as the damage amount and modes. These were thought to be utilized to predict the decrease of mechanical properties and also to help mitigate impact damage of composite structures.

• Composites Research
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• 제24권2호
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• pp.38-45
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• 2011

본 논문에서는 유리섬유 강화 복합재 적층판으로 이루어진 단일층 Dallenbach layer의 전파흡수체의 최적화 기법을 제시하고 그 성능을 분석하였다. 복합재 적층판의 전기적 특성을 제어하기 위해서 탄소나노튜브(CNT)를 혼합한 프리프레그를 사용하였다. 최적화 설계 기법은 유전자 알고리즘을 사용하였으며, 이를 이용하여 다양한 주파수에서 흡수체를 설계하고, 복합재의 두께 및 CNT 함유율을 최적화하였다. CNT 함유율의 최적화를 위해서는 복합재의 복소 유전율의 수치적 모델이 사용되었다. 전파흡수체의 최적설계에서 주파수에 따라서 CNT 함유율은 비례하여 증가하고, 흡수체의 두께는 반비례하여 감소한다. 흡수체의 -10 dB 흡수대역폭은 흡수체가 설계된 중심주파수에 비례하여 증가한다. 설계된 흡수체의 검증을 위해서 10 GHz에서 중심주파수를 갖는 흡수제를 제조하고 그 성능을 평가하였다. 복합재 적층판의 복소 유전율과 전파흡수체의 반사손실은 벡터회로망분석기와 7 mm 동축관을 이용하여 측정하였다. 복합재의 두께와 복소 유전율에 있어서의 측정된 값과 예측치의 차이에 의해서 중심주파수의 이동, 중심주파수에서의 반사손실의 감쇄, 흡수대역폭의 감소가 발생하였다.

• 비파괴검사학회지
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• 제28권3호
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• pp.245-253
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• 2008

A precise description of the material is a key point to obtain reliable results when using wave propagation codes. In the case of multipass welds, the material is very difficult to describe due to its anisotropic and heterogeneous properties. Two main advances are presented in the following. The first advance is a model which describes the anisotropy resulting from the metal solidification and thus the model reproduces an anisotropy that is correlated with the grain orientation. The model is called MINA for modelling anisotropy from Notebook of Arc welding. With this kind of material model1ing a good description of the behaviour of the wave propagation is obtained, such as beam deviation or even beam division. But another advance is also necessary to have a good amplitude prediction: a good quantification of the attenuation, particularly due to grain scattering, is also required as far as attenuation exhibits a strong anisotropic behaviour too. Measurement of attenuation is difficult to achieve in anisotropic materials. An experimental approach has been based both on the decomposition of experimental beams into plane waves angular spectra and on the propagation modelling through the anisotropic material via transmission coefficients computed in generally triclinic case. Various examples of results are showed and also some prospects to continue refining numerical simulation of wave propagation.

• 소성∙가공
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• 제29권3호
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• pp.157-162
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• 2020

Blind rivet nuts are increasingly used in automotive for the joining of sheets. Their application, however, requires appropriate design guides to prevent catastrophic events arising from the failure of joints. In this study, the shaft shape of a frequently used M8 blind rivet nut is optimized based on 3D numerical analysis of the blind rivet nut considering the characteristics of thread. The thread needs to be modeled to suitably consider the fastening of the M8 bolt after the crimping process. FE analysis showed that while the friction in the contact between crimp flange and plate has no significant effect on the crimp geometry, shaft thickness (t) and shaft height (h) are the most significant design variables. The parameter study including various combinations of t and h reveals that they affect the gap (the distance between the crimped flange and the plate that develops through riveting) and the load acting on the plate. The gap is an indicator of the tightening force. It is found that t is inversely proportional to the gap, and proportional to the load, whereas h is proportional to the gap and inversely proportional to the load. Based on our FE analysis results, we propose the range 0.062 < t/h < 0.1 to ensure sufficient fastening (high clamping load, small gap) of the M8 blind rivet nut. The design guide for determining the t/h ratio proposed in this study can be used for general quantitative analysis of the size and the t/h ratio of blind rivet nuts.

• 응용통계연구
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• 제18권1호
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• pp.83-98
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• 2005

다변량 자료를 분석하는 데 있어서 관측 개체들의 분포적 양태를 파악하는 것은 자료 특성의 이해에 도움이 될 뿐만 아니라 이후 모형화 과정에도 큰 도움을 준다. 이를 위하여 다변량자료의 저차원 시각화에 대한 많은 연구가 진행되어 왔다. 그 중 하나가 코호넨(T. Kohonen)의 자기조직화지도(Self-Organizing Map; SOM)이다. SOM은 저차원 그리드 공간에 고차원 다변량 자료를 축약하여 시각적으로 나타내는 비지도 학습법의 일종으로 최근 들어 통계 분석자들이 많은 관심을 가지고 있는 분야이다. 그러나 SOM은 개체공간의 연속형으로 표현되는 개체를 저차원 그리드 공간에 승자노드에 의해 비연속적으로 표현한다는 단점을 지니고 있다. 본 논문에서는 SOM을 통계적 목적으로 사용하기 위해 요구되는 그리드 공간에 개체를 연속적으로 표현하는 방법들을 제안하고 환용 예를 제시 하고자 한다.

• 한국신재생에너지학회:학술대회논문집
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• 한국신재생에너지학회 2009년도 추계학술대회 논문집
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• pp.465-465
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• 2009

Wind power is one of the most reliable renewable energy sources and the installed wind turbine capacities are increasing radically every year. Although wind power has been favored by the public in general, the problem with the impact of wind turbine noise on people living in the vicinity of the turbines has been increased. Low noise wind turbine design is becoming more important as noise is spreading more adverse effect of wind turbine to public. This paper demonstrates the design of 10 kW class wind turbines, each of three blades, a rotor diameter 6.4m, a rated rotating speed 200 rpm and a rated wind speed 10 m/s. The optimized airfoil is dedicated for the 75% spanwise position because the dominant source of a wind turbine blade has been known as trailing edge noise from the outer 25% of the blade. Numerical computations are performed for incompressible flow and for Mach number at 0.145 and for Reynolds numbers at $1.02{\times}10^6$ with a lift performance, which is resistant to surface contamination and turbulence intensity. The objective in the low design process is to reduce noise emission, while sustaining high aerodynamic efficiency. Dominant broadband noise sources are predicted by semi-empirical formulas composed of the groundwork by Brooks et al. and Lowson associated with typical wind turbine operation conditions. During the airfoil redesign process, the aerodynamic performance is analyzed to minimize the wind turbine power loss. The results obtained from the design process show that the design method is capable of designing airfoils with reduced noise using a commercial 10 kW class wind turbine blade airfoil as a basis. The new optimized airfoil clearly indicates reduction of total SPL about 3 dB and higher aerodynamic performance.

• 농업과학연구
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• 제40권2호
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• pp.123-129
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• 2013

An experiment was conducted to evaluate the effects of nitrogen supplementation through urea-molasses multinutrient block (UMMB) on the performance of dairy cows fed good quality forage based diets with rice straw as a night feeding. A total of 10 multiparous crossbred dairy cows in their early lactation were grouped into two categories based on their breed, parity, body weight, milk yield, milk fat and protein contents and daily fed a chopped CO-3 grass (Pennisetum purpureum ${\times}$ Pennisetum americanum; hybrid Napier) ad-libitum, 1 kg of dairy cow concentrate feed during the day time and 5 kg of rice straw (dry matter basis) at night as the basal diet (control) for 5 wk. In addition to the basal diet, the treatment group received 300 g of crushed UMMB daily throughout the experimental period. Cows were milked twice daily and the milk yields were recorded. Milk and feed samples were collected weekly for chemical analysis. Supplementation of UMMB had no significant effects (p>0.05) on straw intake, daily milk yield, contents and yields of milk constituents such as milk fat, protein, lactose and solids-non-fat. In addition, milk urea nitrogen content were not affected (p>0.05) by UMMB supplementation. However, numerical increments in all the parameters measured were observed during the study in cows fed diets supplemented with UMMB. It can be concluded that nitrogen supplied through UMMB had no effects on production performances of dairy cows in this study.

• 전기학회논문지
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• 제64권4호
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• pp.505-514
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• 2015

This paper proposes a probabilistic generation assessment model of renewable energy generators(REGs) considering uncertainty of resources, mainly focused on Wind Turbine Generator(WTG) and Solar Cell Generator(SCG) which are dispersed widely in South Korea The proposed numerical analysis method assesses the one day-ahead generation by combining equivalent generation characteristics function and probabilistic distribution function of wind speed(WS) and solar radiation(SR) resources. The equivalent generation functions(EGFs) of the wind and solar farms are established by grouping a lot of the farms appropriately centered on Weather Measurement Station(WMS). First, the EGFs are assessed by using regression analysis method based on typical least square method from the recorded actual generation data and historical resources(WS and SR). Second, the generation of the REGs is assessed by adding the one day-ahead resources forecast, announced by WMS, to the EGFs which are formulated as third order degree polynomials using the regression analysis. Third, a Renewable Energy Generation Assessment System(REGAS) including D/B of recorded actual generation data and historical resources is developed using the model and algorithm predicting one day-ahead power output of renewable energy generators.

• 한국통신학회논문지
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• 제22권9호
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• pp.2014-2026
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• 1997

본 논문에서는 현재 광대역 고속네트워킹의 핵심기술인 비동기 전송방식(Asynchronous Transfer Mode: ATM)을 사용하는 통신 네트워크에서 무선채널을 이용하여 ATM 셀을 전송할 때에 비트오율 성능, 셀손실확률, 셀오류확률 및 네트워크 성능을 분석하였다. 무선 채널에서의 변조방식으로는 대역폭 효율을 높히기 위하여 16Star QAM방식을 적용하였으며, 무선 채널에서의 성능을 개선하기 위한 채널부호화 기법으로는 Reed-Solomon (R-S)부호, 길쌈부호, R-S/길쌈부호의 인쇄부호를 적용하였으며, 효과적으로 ATM셀을 전송하기 위한 UEP(unequal error protection) 부호화 방안으로 부분 연쇄부호를 제시하고 성능을 분석하였다. 이동 무선 통신채널의 특성인 도플러 영향과 라이시안 페이딩 모델을 고려하였고 수신단에서의 성능을 향상시키기 위하여 최대비 결합 방식의 다이버시티 기법을 적용하였으며, 네트워크 성능분석을 위하여는 무선 ATM셀의 셀 전송효율 및 지연시간을 분석하였다. 성능분석 결과로, 부분 연쇄부호를 적용시 기존의 부호화 기법들에 비하여 약 2dB 이상의 ATM 셀 손실 성능 향상을 기대할 수 있으며, 특별히 낮은 오류확률을 요구할 수록 좋은 성능을 보임을 알 수 있었다. 또한 동일한 성능을 얻기 위하여 적용하는 부호화 기법의 오버헤드 비트를 줄일 수 있는 방안임을 확인하였다. 따라서, 부분연쇄부호와 같이 ATM 셀의 헤더와 payload 부분의 에러 보정능력을 달리 적용하는 부호화 기법을 채택하는 것이 미래의 이동통신망에서의 무선 ATM통신을 위한 유용한 전송방식으로 생각된다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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• pp.671-686
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• 2004

The shock-induced combustion ramjet (shcramjet) is a hypersonic airbreathing propulsion concept which over-comes the drawbacks of the long, massive combustors present in the scramjet by using a standing oblique detonation wave (a coupled shock-combustion front) as a means of nearly instantaneous heat addition. A novel shcramjet combustor design that makes use of wedge-shaped flameholders to avoid detonation wave-wall interactions is proposed and analyzed with computational fluid dynamics (CFD) simulations in this study. The laminar, two-dimensional Navier-Stokes equations coupled with a non-equilibrium hydrogen-air combustion model based on chemical kinetics are used to represent the physical system. The equations are solved with the WARP (window-allocatable resolver for propulsion) CFD code (see: Parent, B. and Sislian, J. P., “The Use of Domain Decomposition in Accelerating the Convergence of Quasihyperbolic Systems”, J. of Comp. Physics, Vol. 179, No. 1,2002, pages 140-169). The solver was validated with experimental results found in the literature. A series of steady-state numerical simulations was conducted using WARP and it was deter-mined by means of thrust potential calculations that this combustor design is a viable one for shcramjet propulsion: assuming a shcramjet flight Mach number of twelve at an altitude of 36,000 m, the geometrical dimensions used for the combustor give rise to an operational range for combustor inlet Mach numbers between six and eight. Different shcramjet flight Mach numbers would require different combustor dimensions and hence a variable geometry system in or-der to be viable.