• 한국산업융합학회 논문집
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• 제25권3호
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• pp.477-491
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• 2022

This study proposed the performance analysis and hydraulic control system design of forklift structure manipulator with 5 joints for untact working in lilited environment. The performance analysis of the control system analyzed the control response to load and pressure fluctuations. The reliability of proposed control system was verified by simulation test under the various condition.

• 대한토목학회논문집
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• 제30권1D호
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• pp.1-10
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• 2010

고속도로 영업소의 경우 하이패스차량과 일반TCS이용차량간의 혼용 및 차로변경으로 인한 상충이 발생하는 구간으로 안전성에 대한 검토가 필요한 구간이다. 본 연구에서는 영업소 진출부에 설치된 중앙하이패스 이용차량과 일반차로 이용차량간의 상충 및 사고위험성을 현장비디오촬영 및 상충분석을 통해 알아보았다. 차량속도와 상대속도 및 상충으로 인한 차량 감속시간 등을 분석한 결과 하이패스이용차량과 일반TCS이용차량간의 상대속도가 클수록 상충으로 인한 차량 급감속이 발생한다는 문제점을 파악하였으며, 중앙 하이패스 설치시 상충 발생 위치 및 차로 운영형태에 따라 상충빈도 및 상대속도가 다름을 확인할 수 있었다. TA(Time to Accident)분석 결과, 고속도로 영업소 중앙 하이패스 설치시 차량간 상대속도, 상충위치 및 빈도에 따른 상충시 하이패스 차량의 급감속 및 감속시간이 큼에 따라 사고위험이 높은 것으로 분석되었다. 또한 합류 시점부가 영업소 진출부와 가까울수록 TA분석값이 낮은 것으로 분석되어 전반적으로 속도차이를 줄여 안전성을 증대시켜야 함을 알 수 있었다. 본 연구에서는 영업소 진출부 중앙 하이패스 설치로 발생하는 상대속도차에 의한 상충으로 급감속 및 사고를 억제함으로서 영업소 중앙 하이패스 차로 설치시 안전성을 높여줄 수 있을 것으로 기대된다.

• 한국전산유체공학회지
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• 제19권4호
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• pp.20-28
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• 2014

An efficient solution algorithm for simulating free surface problem is presented. Navier-Stokes equations for variable density incompressible flow are employed as the governing equation on Cartesian meshes. In order to describe the free surface motion efficiently, VOF(Volume Of Fluid) method utilizing THINC(Tangent of Hyperbola for Interface Capturing) scheme is employed. The most time-consuming part of the current free surface flow simulations is the solution step of the linear system, derived by the pressure Poisson equation. To solve a pressure Poisson equation efficiently, the PCG(Preconditioned Conjugate Gradient) method is utilized. This study showed that the proper application of the preconditioner is the key for the efficient solution of the free surface flow when its pressure Poisson equation is solved by the CG method. To demonstrate the efficiency of the current approach, we compared the convergence histories of different algorithms for solving the pressure Poisson equation.

• 한국항공우주학회지
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• 제35권8호
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• pp.661-669
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• 2007

지면효과에 대한 수치해석을 위한 격자생성 과정에서 발생하는 어려움을 해소하기 위하여 중첩격자 기법을 이용한 수치해석 기법의 타당성에 대한 연구를 수행하고 그 신뢰성을 검증하였다. 지면효과가 있는 경우와 없는 경우 RAE 101 익형주위의 저속 난류 유동장에 대한 수치해석을 수행하였고 다중블록격자 기법과 중첩격자 기법을 적용한 수치해석 결과를 실험결과와 비교하였다. 이를 통하여 중첩격자 기법을 이용함으로써 지면효과에 대한 수치해석과정을 정확하고 격자생성 문제없이 효과적으로 수행할 수 있음을 보였다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2001년도 춘계 학술대회논문집
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• pp.189-194
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• 2001

In this paper, non-reacting and reacting flowfields were computed using a preconditioned Navier-Stokes solver. The preconditioning technique of Merkle et al. and TVD scheme or Chakravarthy and Osher was employed and the results obtained using developed code have a good agreement with the previous results and experimental data. The preconditioned Wavier-Stokes equation set with low Reynolds number $\kappa-\epsilon$ equation and species continuity equations, are discretized with strongly implicit manner and time integrated with LU-SSOR scheme. For the purpose of treating unsteady problem the duel-time stepping scheme was employed. For the validation of the code in incompressible flow regime, steady driven square cavity flow was considered and calculation result shows reasonably good agreement with the result of incompressible code. Shock wave/boundary layer interaction problem was considered to show the shock capturing performance of preconditioned-TVD scheme. To validate unsteady flow, acoustic oscillation problem was calculated, and supersonic premix flame of $H_2$-air reaction problem which is calculated with turbulence model, 9-species/18-reaction step reaction model, shows reasonable agreement with the previous results. As a result, the preconditioning method has an advantage to calculate incompressible and compressible flow through one code and preconditioned solver easily developed from standard compressible code with minor efforts. But additional computational time and computer memory is required due to preconditioning matrix.

• 대한한의학원전학회지
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• 제18권3호통권30호
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• pp.207-212
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• 2005

통과대진사탁명문지설특징적연구득출이하결론(通過對陳士鐸命門之說特徵的硏究得出以下結論): 1. 명문위선천지화(命門爲先天之火), 차종개념상역가위선천지수화(且從槪念上亦可爲先天之水火). 2. 명문지화가칭지위선천지화(命門之火可稱之爲先天之火), 신화(腎火), 신중지화(腎中之火), 무형지화(無形之火), 진화(眞火), 건화(乾火), 원기(原氣), 음중지화(陰中之火), 수중유양등(水中有陽等); 이명문지수가칭지위선천지수(而命門之水可稱之爲先天之水), 신수(腎水), 신중지수(腎中之水), 무형지수(無形之水), 진수(眞水), 원정(原精), 음중지수(陰中之水), 화중유음등(火中有陰等). 3. 진수가생진화(眞水可生眞火), 진화역가생진수(眞火亦可生眞水), 양자위호생적관계(兩者爲互生的關係). 강조료유형지화(强調了有形之火), 수극화(水克火), 단무형지화(但無形之火), 수생화(水生火). 4. 명문지화시일양함어이음지간적감괘상(命門之火是一陽陷於二陰之間的坎卦象). 5. 인적생명활동고수화이생, 이신중적진화진수지명문시기본원(而腎中的眞火眞水之命門是其本源). 6. 명문시운행십이경맥적주체(命門是運行十二經脈的主體), 시십이경지주(是十二經之主), 차위촉사생성십이관공능적십이관지화원(且爲促使生成十二官功能的十二官之化源), 고위십이관지주(故爲十二官之主). 7. 명문적작용가영향정개십이관(命門的作用可影響整個十二官), 우기시인화생토적관계(尤其是因火生土的關係), 대비적공능적영향갱대(對脾的功能的影響更大). 8. 인적생명지성쇠의고명문지화, 고명문지화고갈즉인적생명장종결(故命門之火枯竭則人的生命將終結). 9. 오곤(吳崑), 장개빈등계승료류하간적주장(張介賓等稽承了劉河間的主張), 기인위자하향상수지제칠절처위시명문(旣認爲自下向上數至第七節處爲是命門), 차처기위소심(此處旣爲小心). 10. 진사탁계승상술학설화조헌가지설(陣士鐸繼承上述學說和趙獻可之說), 주장칠절지방시소심(主張七節之芳是小心), 차인위차처기위명문소재(且認爲此處旣爲命門所在).

• Journal of Chest Surgery
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• 제27권7호
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• pp.563-570
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• 1994

Effect of ischemic preconditioning on left ventricular function after cardiac arrest in isolated rat heart.Ischemic preconditioning reduces infarct size caused by sustained ischemia. However, the effects of preconditioning on post ischemic cardiac function are not well-known. The objective of the present study was to determine whether preconditioning would improve the recovery of left ventricular functions after cardiac arrest in isolated rat heart model.Isolated rat hearts were allowed to equilibrate for 20 minutes and were then subjected to either 5 minutes of global, normothermic transient ischemia [Group 2 and 4] or not [Group 3]. A stabilization period of perfusion lasting 5 minutes after the termination of transient ischemia was followed by a standard global, normothermic 20 minute-ischemia and 35-minute reperfusion challenge [Group 3 and 4]. These following results were odtained.1. The recovery of left ventricular developed pressures showed no significant differences between Group 3 and Group 4 at 50 [P>0.3] and 85 minute [P>0.2].2. Heart rates showed no significant differences throughout all the course of experiment and between groups [P>0.5].3. The recovery of left ventricular maximum dP/dt showed no significant differences between Group 3 and Group 4 at 50 [P>0.1] and 85 minute [P>0.2].4. The recovery of pressure-rate products showed no significant differences between Group3 and Group 4 at 50 [P>0.5] and 85 minute [P>0.1].These results suggest that ischemic preconditioning does not provide significant benefit for the postischemic left ventricular functions in isolated rat hearts.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2009년도 제33회 추계학술대회논문집
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• pp.42-46
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• 2009

고압 조건에서 작동하는 고성능 액체 로켓 엔진에 대한 이해를 위해 초임계 조건의 스월 인젝터에서 액체 산소의 동적 특성이 수치적으로 연구되었다. 난류 수치 모델은 large eddy simulation을 기반으로 하였으며 보존 방정식과 SRK 상태 방정식, Chung의 기법을 포함하고 있다. 또한 수렴 속도의 증가를 위해 예조건화 기법이 적용되었다. 수치 해석 결과는 이상 기체 상태 방정식을 적용한 결과와 비교 되었으며 인젝터 내부와 연소실에서 액상이 존재하는 영역에서의 상태량과 동적 특성의 차이가 관찰되었다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2006년도 추계 학술대회논문집
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• pp.193-198
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• 2006

It takes a lot of time and effort to generate grids for numerical analysis of problems with ground effect because the relative attitude and height of airfoil should be maintained to the ground as well as the inflow. A low Mach number preconditioned turbulent flow solver using the overlap grid technique has been developed and applied to the ground effect simulation. It has been validated that the present method using the multi-block grid gives us highly accurate solutions comparing with the experimental data of the RAE 101 airfoil in an unbounded condition. Present numerical method has been extended to simulate ground effect problems by using the overlapped grid system to avoid tedious work in generating multi-block grid system. An extended method using the overlapped grid has been verified and validated by comparing with results of multi-block method and experimental data as well. Consequently, the overlapped grid method can provide not only sufficiently accurate solutions but also the efficiency to simulate ground effect problems. It is shown that the pressure and aerodynamic centers move backward by the ground effect as the airfoil approaches to the ground.

• 한국전산유체공학회지
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• 제17권1호
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• pp.78-85
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• 2012

Cavitation causes a great deal of noise, damage to components, vibrations, and a loss of efficiency in devices, such as propellers, pump impellers, nozzles, injectors, torpedoes, etc., Thus, cavitating flow simulation is of practical importance for many engineering systems. In this study, a two-phase flow solver based on the homogeneous mixture model has been developed. The flow characteristics around an axisymmetric cylinder were calculated and then validated by comparing with the experimental results in the cavitation water tunnel at the Korea Ocean Research & Development Institute. The results show that this solver is highly suitable for simulating the cavitating flows. After the code validation, the cavity length with changes of water depth, angle of attack and velocity were obtained.. Cavitation inception was also calculated for various operational conditions.