• 대한의용생체공학회:의공학회지
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• 제25권1호
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• pp.71-76
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• 2004

척추 측만증 교정 시 유합 범위에 따른 수술 후 의 효과를 분석하기 위하여 King-Moe type II 형태의 척추 측만증 환자를 대상으로 이에 대한 수학적 유한 요소 모델을 개발하였다. 유한 요소 모델을 이용하여 척추경 나사못을 이용한 고정 및 강봉 감염술 형태의 수술모사를 수행하였으며, 유합 범위를 각기 달리하여 수술 시뮬레이션 후의 척추계의 변화 즉 Cobb 각도, 첨추체 축회전, 흉추 후만각 그리고 늑골고의 변화를 정량적으로 계산하였다. 해석 결과 강봉 감염술의 경우에서 보다 강봉을 척추경 나사못에 연결시키는 과정에서 훨씬 더 많은 Cobb각도의 변화를 얻을 수 있었다. 강봉 감염술 과정에서는 약간의 Cobb각도 감소를 유발시킬 수 있었으나 오히려 척추체 축회전과 늑골 돌출고의 증가를 나타내었다 아울러 강봉과 척추경 나사못의 체결 과정이 척추 후만각 유지에도 큰 역할을 하고 있음을 알 수 있었다. 유합 범위를 변곡 발생 추체의 위치 보다 한 단계씩 길게(T4-12) 하여 60o의 강봉 감염술을 시행하였을 경우 Cobb 각도를 두 배 감소시킬 수 있었으나 급격한 늑골고와 첨추체 축회전량의 증가가 유발되었다. 해석 결과 유합 범위는 만곡 흠추체에서 변곡이 발생되는 위치 보다 한 레벨씩 작게 선정하는 것이 최적의 유합 범위임을 알 수 있었다.

• Journal of Advanced Marine Engineering and Technology
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• 제40권4호
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• pp.270-274
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• 2016

양 벽면이 수축되는 채널에서 ${\vee}/{\wedge}$형 리브의 각도가 열전달에 미치는 효과를 실험적으로 조사하였다. 한 벽면에만 설치된 ${\vee}/{\wedge}$형 리브의 충돌 각은 각각 $30^{\circ}$, $45^{\circ}$, $60^{\circ}$ 그리고 $90^{\circ}$이다. 리브의 높이(e)는 10 mm 그리고 리브 간격(p)과 높이(e)비는 10으로 제작하였다. 길이가 1,000 mm인 시험 부는 입구의 단면적은 $100mm{\times}100mm$, 출구는 $50mm{\times}100mm$으로 제작하였다. 레이놀즈수가 22,000에서 75,000까지의 범위에서 실험을 수행하였다. 연구결과 전체적으로 레이놀즈 수가 높을수록 누셀트 수가 컸고, ${\wedge}$형 $45^{\circ}$ 리브가 가장 누셀트 수가 컸다.

• 대한기계학회논문집B
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• 제32권4호
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• pp.300-306
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• 2008

In the present study, the second order response surface method (RSM) is carried out to get optimum thermal design for enhancing heat transfer in a square channel with bleed flow. The RSM is used as an optimization technique. To calculate the heat transfer, RNG k-epsilon model and enhanced wall function are used. To design optimum rib turbulators, two design variables such as attack angle of rib $({\alpha})$ and rib pitch-to-rib height ratio (p/e) are optimized. In these analyses, the channel inlet Reynolds number was fixed at 10,000 in both non-bleeding and bleeding cases. The response surfaces of two design variables are constructed in cases with and without bleed flow. As a result, the optimum (or highest) heat transfer values are almost the same in ranges of two cases with and without bleed flow. However, the friction losses in the case with bleed flow are lower than those without bleed flow.

• Geomechanics and Engineering
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• 제25권3호
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• pp.233-243
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• 2021

Rib spalling is a major issue affecting the safety of steeply inclined coal seam. And the failure coal face and support system can be affected with each other to generate a vicious cycle along with inducing large-scale collapse of surrounding rock in steeply inclined coal seam. In order to analyze failure mechanism and propose the corresponding prominent control measures of steeply inclined coal working face, mechanical model based on coal face-support-roof system and mechanical model of coal face failure was established to reveal the disaster mechanism of rib spalling and the sensitive analysis of related factors was performed. Furthermore, taking 3402 working face of Chen-man-zhuang coal mine as engineering background, numerical model by using FLAC3D was built to illustrate the propagation of displacement and stress fields in steeply inclined coal seam and verify the theory analysis as mentioned in this study. The results show that the coal face slide body in steeply inclined working face can be observed as the failure height of upper layer smaller than that of lower layer exhibiting with an irregular quadrilateral pyramid shape. Moreover, the cracks were originated from the upper layer of sliding body and gradually developed to the lower layer causing the final rib spalling. The influence factors on the stability of coal face can be ranked as overlying strata pressure (P) > mechanical parameters of coal body (e.g., cohesion (c), internal fraction angle (φ)) > support strength (F) > the support force of protecting piece (F') > the false angle of working face (Θ). Moreover, the corresponding control measures to maintain the stability of the coal face in the steeply inclined working face were proposed.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 추계학술대회논문집B
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• pp.22-29
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• 2001

The present study investigates the effects of various rib arrangements and rotating on heat/mass transfer in the cooling passage of gas turbine blades. The cooling passage has very complex flow structure, because of the rib turbulator and rotating effect. Experiments and numerical calculation are conducted to investigate the complex flow structures and heat transfer characteristics; the numerical computation is performed using a commercial code, FLUENT ver.5, to calculate the flow structures and the experiments are conducted to measure heat/mass transfer coefficients using a naphthalene sublimation technique. For the rotating duct tests, the test duct, which is the cross section of is $20mm\times40mm$ (the hydraulic diameter, $D_h$, of 26.7 mm, has two-pass with $180^{\circ}$ turning and the rectangular ribs on the wall. The rib angle of attack is $70^{\circ}$ and the maximum radius of rotation is $21.63D_h$. The partition wall has 10 mm thickness, which is 0.5 times to the channel width, and the distance between the tip of the partition wall and the outer wall of the turning region is 26.7 mm $(1D_h)$. The turning effect of duct flow makes the very complex flow structure including Dean type vortex and high turbulence, so that the heat/mass transfer increases in the turning region and at the entrance of the second pass. The Coriolis effect deflects the flow to the trailing surface, resulting in enhancement of the heat/mass transfer on the trailing surface and reduction on the leading surface in the first pass. However, the opposite phenomena are observed in the second pass. The each rib arrangement makes different secondary flow patterns. The complex heat/mass transfer characteristics are observed by the combined effects of the rib arrangements, duct rotation and flow turning.

• 소성∙가공
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• 제28권3호
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• pp.145-153
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• 2019

The objective of this study is to analyze the mechanical splicing characteristic of the threaded bar according to the contact conditions of the transverse rib. In order to consider the contact conditions of the rib, selection of the main variables including the gap of the core diameter ($l_c$), rib angle (${\theta}$), and the number of contacts ($C_N$) of transverse rib was done. So as to analyze the splicing characteristic of the D51 threaded bar, a finite element (FE) simulation of the tensile test was conducted using the designed D51 threaded bar and coupler. Through FE simulation results, it was verified that the mechanical slicing characteristics varied based on the main design variables ($l_c$, ${\theta}$, and $C_N$). It was further confirmed that it was important to determine the $C_N$ in consideration of $l_c$. Additionally, the tensile test results of the D25 and D51 threaded bar combined with the couplers were similar to FE simulation results. Furthermore, to quantitatively evaluate FE simulation and test results, the calculation equation for the contacted projection area ratio (R) of the transverse rib was proposed. To secure a mechanical splicing joint of the threaded bar, it was established that the R calculated using the proposed equation had to be greater or equal to 40%.

• 한국방사선학회논문지
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• 제13권7호
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• pp.979-986
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• 2019

본 연구는 Rib Rando Phantom을 이용하여 겨드랑 첫 번째, 두 번째 갈비뼈 골절이 선예하게 나타나는 영상의 검사방법을 연구하였다. 팬톰의 자세와 엑스선관 각도를 수직, 머리쪽 5°, 다리쪽 5°로 변경하여 검사하였다. 획득한 영상을 방사선사가 주관적으로 영상평가 하였으며, 평가 데이터를 SPSS ver. 3.0으로 분석하였다. ImageJ Program을 이용하여 신호대잡음비(SNR)를 계산하였다. 그 결과 Cronbach Alpha 값이 0.789로 유의하게 높았다. 신호대잡음비(SNR)의 결과는 갈비뼈 앞쪽의 경우 엑스선관을 머리쪽으로 5° 기울여 검사 시 6.038, 갈비뼈 뒤쪽의 경우 엑스선관을 다리쪽으로 5° 기울여 검사 시 7.860으로 가장 높았다. 겨드랑 갈비뼈의 촬영기법으로 앞쪽 검사는 골절된 부위를 거상하고 엑스선관 각도를 머리쪽으로 5° 주며, 뒤쪽 검사는 골절된 부위를 밀착하여 엑스선관 각도를 발쪽으로 5° 기울여 검사한다면 선예한 영상을 얻을 수 있을 것으로 사료된다.

• 대한조선학회논문집
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• 제47권3호
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• pp.462-468
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• 2010

A new course keeping controller for RIB(Rigid Inflatable Boat)-type USV(Unmanned Surface Vehicle) is developed using pilot's steering pattern. A pilot's simple steering pattern is found out from various course change tests. It is used to course keeping algorithm, suitable for large course change more than 60 degrees. To validate the course keeping controller, sea trial tests are conducted. From sea trial test, new course keeping controller shows good performance with less overshoot, maximum roll angle less than $20^{\circ}$, which makes it possible that fast course changes without slip motion of USV.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 1999년도 봄 학술발표회 논문집
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• pp.343-350
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• 1999

Orthotropic steel bridge decks are potentially liable to cause fatigue cracks due to weld defects, residual stresses, and in-plane or out-of-plane stresses. In particular, the cracks propagated through deckplate in longitudinal rib to deckplate joints occur at weld toe and weld root due to stress concentrations. Numerical parametric studies are performed to show the Influence of the parameters on the stress concentration at the connection between the longitudinal rib and the deckplate. The parameters include root gap, toe angle $\theta$, toe radius $\rho$, and weld penetration. This study provides a fundamental point for the improvement of fatigue resistance and the estimation of the fatigue crack propagation in wekded joint details.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2007년도 춘계학술대회B
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• pp.2384-2389
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• 2007

The 2nd order response surface method (RSM) has been carried out to get optimum thermal design for enhanced heat transfer on square channel with bleed holes. The RSM was used as an optimization technique with Reynolds-averaged navier-stokes equation. Turbulence model for heat transfer analysis used RNG k-epsilon model. The wall function used enhanced wall function. Numerical local heat transfer coefficients were similar to the experimental tendency. Two design variables such as attack angle of rib (${\alpha}$), rib pitch-to-rib height ratio (p/e) were chosen. Operation condition considered bleeding ratio per bleed hole ($BR_{hole}$). A response surface were constructed by the design variables and operation condition. As a result, adjusted $R^2$ was more than 0.9. Optimization results of various objective function were similar to heat transfer in channel with and without bleed flow. But friction factor was lower than channel without bleed flow.