• 한국구조물진단유지관리공학회 논문집
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• 제20권6호
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• pp.65-72
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• 2016

염해에 콘크리트 구조물의 내구수명 평가는 매우 중요한데, 결정론적 방법 및 확률론적 방법에서 평가된 결과는 큰 차이를 보이고 있다. 본 연구에서는 시간의존형 확산계수와 고정 확산계수를 고려하여 내구수명을 모사하였다. 기본확산계수, 콘크리트 피복두께, 표면염화물량을 3조건으로 분류하여 각 평가방법에 따라 변화하는 내구적 파괴확률과 내구수명을 평가하였다. 시간의존형 확산계수의 도입을 통하여 두 방법 간의 차이를 감소시킬 수 있었으며, 합리적인 해석결과를 유도할 수 있었다. 염화물 확산계수가 $2.5{\times}10^{-12}m^2/sec$에서 $7.5{\times}10^{-12}m^2/sec$으로 증가할 때 내구수명은 25.5~35.6%수준으로 감소하였으며, 피복두께가 75 mm에서 125 mm로 증가할 경우, 267~311%로 내구수명은 증가하였다. 또한 표면염화물량이 $5.0kg/m^3$에서 $15.0kg/m^3$으로 변화할 때, 내구수명은 40.9~54.5% 수준으로 감소하였다. 피복두께의 변화에 따른 내구수명의 변화는 기본확산계수 및 표면염화물에 비하여 8~10배정도 크게 평가되었으며 내구수명 확보를 위한 중요한 인자임을 알 수 있다.

• 대한조선학회논문집
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• 제35권3호
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• pp.1-13
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• 1998

본 논문에서는 9절점 라그란지안(Lagrangian) 곡면요소를 바탕으로 한 고차경계요소법(Higher-order Boundary Element Method)을 사용하여 자유수면 아래에서 일정한 속도로 전진하는 3차원 수중익에 대한 유체역학적 특성을 연구하였다. 수치계산법에 있어서 자유수면의 계산결과를 개선하기 위해 겹2차 스플라인(bi-quadratic spline)기법을 도입하였다. 수치기법의 검증에서 잠수된 구와 구형체에 대한 해석해와 수치계산 결과가 잘 일치함을 볼 수 있었다. 수중익 문제에 대한 적용성과 그 타당성을 검증하기 위해서 가로-세로비(aspect ratio; A.R.)가 4인 NACA641A412 단면을 가신 3차원 수중익 주위 유동을 해석하였다. 속도가 일정할 때 받음각(angle of attack)과 잠수깊이 변화에 따른 Wadlin et al.[28]의 양력과 항력 계측 실험결과와 비교하였으며, 각각의 경우에 대해 본 수치계산 결과들이 실험결과와 비교적 잘 일치하는 것을 볼 수 있었다. 가로-세로비 4의 NACA0012단면을 가지는 수중익에 대한 계산결과에서는 수중익에 작용하는 양력과 항력에 미치는 자유수연의 영향을 고찰하였으며, 서로 다른 속도와 잠수깊이에서 수중익에 의해 발생하는 자유수면의 변위변화를 고찰하였다.

• 콘크리트학회논문집
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• 제18권1호
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• pp.125-132
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• 2006

최근 들어 툭별한 물리적 방법을 사용하지 않고 내구성능이 저하된 콘크리트의 성능을 회복시키는 방법의 일환으로서 콘크리트 표면보호재에 대한 관심이 높아지고 있다. 표면보호는 직접적인 의미로서는 콘크리트 구조물의 표면을 보호하는 것뿐만아니라 다양한 열화요인의 침투를 억제함으로서 내부의 콘크리트 및 철근의 열화를 억제하여 콘크리트 구조물을 보호하게 된다. 이와 같은 표면보호재 중 함침계 표면보호재는 콘크리트 표면층의 공극에 충전 혹은 생성물을 석출시켜 치밀한 층으로 하느 충전계와 콘크리트 표면층의 외부 및 내부표면의 성질을 개선하는 표면계로 분류하는 것이 가능하다. 따라서 본 연구는 규플르오르화염을 주성분으로 하는 표면형 함침계 표면보호제 도포에 의한 콘크리트 표면의 세공구조의 변화 및 중성화, 염해, 화학적 침식 등의 내구성 향상을 실험실증적으로 검토함으로서 콘크리트 구조물의 내구성향상 방안을 제시하고자 한다. 그 결과, 표면보호제를 도포함으로서 모든 물시멘트비에서 도포전과 비교하여 전세공용적이 감소하고 있으며, 특히 50nm이상의 비교적 큰 세공경인 모세관공극의 용적이 감소함으로서 물흡수성, 중성화 저항성, 내황산성, 염소이온침투 저항성 등의 내구성 향상에 기여하는 것으로 나타났으며, 그 효과는 물시멘트비가 클수록 높게 나타났다.

• International Journal of Aeronautical and Space Sciences
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• 제15권4호
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• pp.366-373
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• 2014

A conceptual design of a three-surface strike fighter was studied and stealth performance was taken into account to enhance survivability and battle effectiveness. CATIA was used to design the aircraft's three-dimensional prototype model and the weapon carriage arrangement was also studied. The aircraft's RCS characteristics and distributions under X, S, C, and L bands were simulated using the RCSPlus software, which is based on the PO method. Pressure and velocity distributions of the flow field were also simulated using CFD. A turbulence model was based on standard $k-{\varepsilon}$ function and N-S functions were used during the CFD computation. Lift coefficients, drag coefficients, and lift-to-drag ratio were obtained by aerodynamic simulation. The results showed that: (1) the average value of head-on RCS between ${\pm}30^{\circ}$ is below -3.197 dBsm, and (2) the lift coefficient is 0.34674, the drag coefficient is 0.04275, and the lift-to-drag ratio is 8.11087 when the attack angle is $2.5^{\circ}$.

• 제어로봇시스템학회논문지
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• 제9권4호
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• pp.329-339
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• 2003

A neural network based adaptive controller design method is proposed for reconfigurable flight control systems in the presence of variations in aerodynamic coefficients or control effectiveness decrease caused by control surface damage. The neural network based adaptive nonlinear controller is developed by making use of the backstepping technique for command following of the angle of attack, sideslip angle, and bank angle. On-line teaming neural networks are implemented to guarantee reconfigurability and robustness to the uncertainties caused by aerodynamic coefficients variations. The main feature of the proposed controller is that the adaptive controller is designed with assumption that not any of the nonlinear functions of the system is known accurately, whereas most of the previous works assume that only some of the nonlinear functions are unknown. Neural networks loam through the weight update rules that are derived from the Lyapunov control theory. The closed-loop stability of the error states is also investigated according to the Lyapunov theory. A nonlinear dynamic model of an F-16 aircraft is used to demonstrate the effectiveness of the proposed control law.

• 한국해양공학회지
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• 제22권5호
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• pp.44-51
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• 2008

The planning and design of coastal structures against wave attack is required to accurately predict wave transformation, wave run-up, and fluid. particlevelocities an a slope. On tire other hand, in tire swash and surf zones of a natural beach, where coastal erosion and accretion occur at tire land-sea boundary, hydrodynamic analysis is essential. In this study, a RBREAK2 numerical model was created based on the nonlinear shallow water equation and laboratory measurements were carried out in terms of tire free surface elevations and velocities for tire cases of regular and irregular waves on 1 : 10 and 1 : 5 impermeable slopes. The data were used to evaluate tire applicability and limitations of tire RBREAK2 numerical model. The numerical mode1 could predict tire cross-shore variation of the wave profile reasonably well, but showed more accurate results for slopes that were steeper than 1 : 10. Except near tire wave crest, tire computed depth averaged velocities could represent tire measured profile below tire trough level fairly well.

• 설비공학논문집
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• 제12권9호
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• pp.843-852
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• 2000

The flow characteristics and the heat transfer rate on a surface by interaction of a pair of vortices were studied experimentally. The test facility consisted of a boundary-layer wind tunnel with a vortex introduced into the flow by half-delta winglet protruding from the surface. In order to control the strength of the longitudinal vortices, the angles of attack of the vortex generators were varied from $\pm20\;degree\;to\;\pm45$ degree, but spacings between the vortex generators were fixed to 4 cm. The 3-dimensional mean velocity measurements were made using a five-hole pressure probe. Heat transfer measurements were made using the thermochromatic liquid to provide the local distribution of the heat transfer coefficient. By using the method mentioned above, the following conclusions were obtained from the present experiment. The boundary layer was thinned in the regions where the secondary flow was directed toward the wall and thickened where it was directed away from the wall. The peak augmentation of the local heat transfer coefficient occurred in the downwash region near the point of minimum boundary-layer thickness.

• 한국염색가공학회지
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• 제18권4호
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• pp.37-42
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• 2006

Two kinds of sea-island type polyester ultramicro fibers (fiber fineness : 0.01 and 0.05 denier) were treated with NaOH varying time and concentration. Surface morphology of the treated fibers with alkaline weight loss was observed by SEM. The treated effects were investigated by measuring density, melting temperature, and X-ray diffraction patterns. The surface morphology of the polyester ultramicro fiber was changed by NaOH concentration. Weight loss of 0.01d fiber was much larger than that of 0.05d fiber. Density and crystallinity were increased with weight loss of fiber. After the weight loss had finished, the density and crystallinity were decreased because of attack of island partition of the fiber. A melting temperature$(T_m)$ is $250^{circ}$ at untreated fiber on the whole and in 0.05d fiber the $(T_m)$ is $252^{circ}$ at untreated. In 0.01d fiber the $(T_m)$ was increased with weight loss of fiber.

• Advances in aircraft and spacecraft science
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• 제2권1호
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• pp.45-56
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• 2015

The attitude aerodynamic control is an important subject in the design of an aerospace plane. Usually, at high altitudes, this control is fulfilled by thrusters so that the implementation of an aerodynamic control of the vehicle has the advantage of reducing the amount of thrusters fuel to be loaded on board. In the present paper, the efficiency of a wing-flap has been evaluated considering a NACA 0010 airfoil with a trailing edge flap of length equal to 35% of the chord. Computational tests have been carried out in hypersonic, rarefied flow by a direct simulation Monte Carlo code at the altitudes of 65 and 85 km, in the range of angle of attack 0-40 deg. and with flap deflection equal to 0, 15 and 30 deg.. Effects of the flap deflection have been quantified by the variations of the aerodynamic force and of the longitudinal moment. The shock wave-boundary layer interaction and the shock wave-shock wave interaction have been also considered. A possible interaction of the leading edge shock wave and of the shock wave arising from the vertex of the convex corner, produced on the lower surface of the airfoil when the flap is deflected, generates a shock wave whose intensity is stronger than those of the two interacting shock waves. This produces a consistent increment of pressure and heat flux on the lower surface of the flap, where a thermal protection system is required.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2000년도 유체기계 연구개발 발표회 논문집
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• pp.359-365
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• 2000

Port facilities and marine structures used in marine environment were encountered to corrosion damages because of the influence of $Cl^-$. Generally, to protect these accidents, mainly applied anti-corrosion paint and epoxy coating. But it was still remained erosion-corrosion damage such as impingement erosion, cavitation erosion, deposit attack. There was needs to develope the new coating materials to protective those corrosion damages. This paper, polyester glass flake, vinylester glass flake lining and epoxy coating for SS were investigated electrochemical tests and cavitation erosion test for corrosion behaviour under sea water. The main results obtained are as follows, 1) Surface of epoxy coating appear erosion pin hole but surface of polyester glass flake and vinylester glass flake lining do not appear erosion pin hole after impingement-cavitation erosion test in sea water. 2) Weight loss of polyester glass flake and vinylester glass flake lining do not occur after impingement-cavitation erosion test in sea water. 3) Corrosion current density of polyester glass flake lining less drained than epoxy coating and substrate under corrosion potential.. 4) Corrosion current density of vinylester glass flake lining with three coating less drained than that of polyester glass flake lining with two coating.