• Title/Summary/Keyword: RAM model

검색결과 319건 처리시간 0.025초

RAM 성장모니터링을 위한 실용적인 신뢰성 성장관리 (Practical Reliability Growth Management for RAM Growth Monitoring)

  • Jung Won
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2005년도 추계학술대회 논문집
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    • pp.258-263
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    • 2005
  • The purpose of this research is to present a practical method for efficiently monitoring a reliability growth process using AMSAA(Army Materiel Systems Analysis Activity) reliability growth model. The presented method is viable for identifying failure modes, incorporating design changes and monitoring reliability progress on an on-going basis during the early stages of a product development program. According to the Application Guide for EN 50126(RAM part for Rolling Stock), reliability growth monitoring is essential part of the main tasks of design phase in RAM growth monitoring. Implementation of reliability growth management program will provide very useful information on concept selection, product/process reliability, and cost effectiveness without too much time, money and engineering effort being spent on the development of failure suspect parts.

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유도무기체계 RAM분석을 위한 ILS M&S 설계 (Design of ILS M&S for RAM Analysis in Guided Weapon System)

  • 이용빈;이동욱;이주형;엄천섭;박장원
    • 한국시뮬레이션학회논문지
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    • 제24권2호
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    • pp.19-29
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    • 2015
  • 국방분야에서 M&S 기법은 분석, 훈련, 획득 등 다양한 목적으로 활용되고 있으며 그 중요성은 더욱 증가하고 있다. 무기체계의 종합군수지원(ILS)요소 개발을 위한 RAM분석 시 M&S 기법을 활용하면 수리적인 기법만으로는 분석하기 어려운 시스템의 다양한 변수와 제약사항을 고려한 분석이 가능하다. 무기체계의 RAM분석을 위한 ILS M&S도구를 설계하기 위해서는 M&S의 목적 설정, 무기체계의 특성 및 유사 M&S Tool 기능 분석 등의 활동이 선행되어야 하며 이를 바탕으로 실제 현실을 프로그램으로 구현하기 용이한 형태의 수학적, 논리적 언어로 모델링해야 한다. 본 논문에서는 'OO유도무기체계'의 배치부터 폐기 시까지 발생하는 운용, 저장, 점검, 고장발생, 정비 등 제반 군수지원활동을 모의하여 유도무기체계의 수명주기 동안의 RAM 특성을 예측, 분석할 수 있는 M&S 도구의 모델링 과정을 제시하고자 하며 이는 유사 M&S 도구의 개발 시 참고자료로도 활용 가능할 것이다.

항공사진분석 자료를 이용한 2차원 하천흐름 해석모형의 검증 (Verification of Two Dimensional Hydrodynamic Model Using Velocity Data from Aerial Photo Analysis)

  • 서일원;김성은
    • 대한토목학회논문집
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    • 제31권6B호
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    • pp.515-522
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    • 2011
  • 수리해석 모형들은 하천의 흐름에 대한 연구에 이용되거나, 수공구조물의 설계 및 하천의 설계 등 실무에 널리 사용되고 있다. 이들 수리해석 모형은 실측자료를 통한 보정이 필요하나, 홍수시 유속을 측정하는 것 자체가 위험한 작업이기 때문에 홍수시 하천의 2차원 유속분포에 대한 실측자료가 전무한 실정이다. 이러한 이유로 2차원 수치모형의 결과는 보통 몇 개 지점의 실측된 자료를 비교함으로써 보정 및 검증을 실시하고 있다. 더욱이 설계 홍수량에 대한 모형의 보정은 1차원 모형인 HEC-RAS의 모의결과를 이용하여 보정하고 있다. 본 연구에서는 일본의 토네강(Tone river)에서 홍수시 촬영한 항공사진을 분석하여 추출한 유속벡터 자료를 이용하여 하천설계 실무 및 연구 등에 널리 사용되어지고 있는 2차원 수치모형인 RAMS의 RAM2, SMS의 RMA2와 1차원 모형인 HEC-RAS 모형의 검증을 실시하였다. 또한, HEC-RAS결과를 이용한 2차원 모형의 보정에 대한 타당성을 검토하였다. 검토결과, HEC-RAS 및 RAM2, RMA2 모형의 수위모의 결과 모두 관측점의 수위와 비슷한 결과을 보이고 있었으나, 유속모의의 경우 고수부지에서의 2차원 모형에 의한 유속결과와 항공사진으로부터 추출된 유속결과가 차이를 보이고 있었다. 또한, 1차원 모형에 의한 결과와 항공사진으로부터 추출된 유속장을 단면평균한 유속과 비교한 결과 큰 오차가 발생하고 있는 것으로 나타났다.

The impact of ram pressure on the multi-phase ism probed by the TIGRESS simulation

  • Choi, Woorak;Kim, Chang-Goo;Chung, Aeree
    • 천문학회보
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    • 제43권2호
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    • pp.33.1-33.1
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    • 2018
  • Ram pressure stripping by intracluster medium (ICM) can play a crucial role in galaxy evolution in the high-density environment as seen by many examples of cluster galaxies. Although much progress has been made by direct numerical simulations of galaxies (or a galaxy) as a whole in a cluster environment, the interstellar medium (ISM) in galactic disks is not well resolved to understand responses of the ISM in details. In order to overcome this, we utilize the TIGRESS simulation suite that focuses on a local region of galactic disks and resolves key physical processes in the ISM with uniformly high resolution. In this talk, we present the results from the solar neighborhood TIGRESS model facing the ICM winds with a range of ram pressures. When ram pressure is weaker than and comparable to the ISM weight, the ICM winds simply reshape the ISM to the one-sided disk, but star formation rates remain unchanged. Although there exist low-density channels in the multiphase ISM that allow the ICM winds to penetrate through, the ISM turbulence quickly closes the channels and prevents efficient stripping. When ram pressure is stronger than the ISM weight, a significant amount of the ISM can be stripped away rapidly, and star formation is quickly quenched. While the low-density gas is stripped rapidly, star formation still occurs in the extraplanar dense ISM (1-2kpc away from the stellar disk). Finally, we quantify the momentum transfer from the ICM to the ISM using the mass-and momentum-weighted velocity distribution functions of each gas phase.

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M&S를 활용한 RAM-C 기반 최적 정비 개념 설정 방안 연구 (A Study on the Method for Setting the Optimal Maintenance Concept based on RAM-C Using Modeling & Simulation)

  • 김경록;이기원;정준;차종한
    • 한국군사과학기술학회지
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    • 제25권5호
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    • pp.530-538
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    • 2022
  • Recently, the R&D of weapon systems has been strengthened in terms of economic cost management throughout the entire life cycle from performance. This study proposes the method for setting the optimal maintenance concept based on RAM-C in weapon system acquisition stage by calculating the operation & maintenance cost as well as reliability, availability, and maintainability. First, we design a simulation model for analysis of weapon system logistic supportability. In addition, information such as weapon system Part Breakdown Structure, operation & maintenance system, cost, and etc for simulation analysis, is applied. Based on the obtained simulation results, the optimal plan is selected among alternatives designed with various maintenance concepts through normalization and weight setting. It is expected to be of technical help in the application of RAM-C in the weapon system acquisition stage.

Expansion Tube 내의 램 가속기 유동장의 수치 연구 (Numerical Investigation of Ram Accelerator Flow Field in Expansion Tube)

  • 최정열;정인석;윤영빈
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 1997년도 제8회 학술강연회논문집
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    • pp.43-51
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    • 1997
  • Steady and unsteady numerical simulations are conducted for the experiments performed to investigate the ram accelerator flow field by using the expansion tube facility in Stanford University. Navier-Stokes equations for chemically reacting flows are analyzed by fully implicit and time accurate numerical methods with Jachimowski's detailed chemistry model for hydrogen-air combustion involving 9 species and 19 reaction steps. Although the steady state assumption shows a good agreement with the experimental schlieren and OH PLIF images for the case of $2H_2$+$O_2$+$17N_2$, it fails in reproducing the combustion region behind the shock intersection point shown in the case of $2H_2$+$O_2$+$12N_2$, mixture. Therefore, an unsteady numerical simulation is conducted for this case and the result shows all the detailed flow stabilization process. The experimental result is revealed to be an instantaneous result during the flow stabilization process. The combustion behind the shock intersection point is the result of a normal detonation formed by the intersection of strong oblique shocks that exist at early stage of the stabilization process. At final stage, the combustion region behind the shock intersection point disappears and the steady state result is retained. The time required for stabilization of the reacting flow in the model ram accelerator is found to be very long in comparison with the experimental test time.

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반응면 기법을 이용한 램 가속기 최적설계에 관한 연구 (Ram Accelerator Optimization Using the Response Surface Method)

  • 전용희;전권수;이재우;변영환
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2000년도 춘계 학술대회논문집
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    • pp.159-165
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    • 2000
  • In this paper, numerical study has been done for the improvement of the superdetonative ram accelerator performance and for the design optimization of the system. The objective function to optimize the premixture composition is the ram tube length required to accelerate projectile from initial velocity $V_o$ to target velocity $V_e$. The premixture is composed of $H_2,\;O_2,\;N_2$ and the mole numbers of these species are selected at design variables. RSM(Response Surface Methodology) which is widely used for the complex optimization problems is selected as the optimization technique. In particular, to improve the non-linearity of the response and to consider the accuracy and efficiency of the solution, design space stretching technique has been applied. Separate sub-optimization routine is introduced to determine the stretching position and clustering parameters which construct the optimum regression model. Two step optimization technique has been applied to obtain the optimal system. With the application of stretching technique, we can perform system optimization with a small number of experimental points, and construct precise regression model for highly non-linear domain. The error to compared with analysis result is only $0.01\%$ and it is demonstrated that present method can be applied more practical design optimization problems with many design variables.

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COMBINED FORWARD-BACKWARD EXTRUSION WITH CONTROLLED REVERSAL RAM MOTION -Effect of Reversal Ram Motion-

  • Hanami S.;Matsumoto R.;Otsu M.;Osakada K.;Hayashida D.
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 2003년도 The 8th Asian Symposium on Precision Forging ASPF
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    • pp.162-166
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    • 2003
  • In combined forward-backward extrusion with controlled forward speed by a counter punch, accurate parts with forward rod can be formed. As an extension of this method, reverse extrusion is proposed, in which the extruded forward rod is pushed back while the main punch is kept at the final position after the forward-backward extrusion process. The experiment is carried out using lead as a model material. With the reverse extrusion method, longer forward rods can be formed without under-filling defect than that by combined extrusion with controlling extrusion speed.

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함정 전·평시 OMS/MP 설정 방법론 연구 및 사례 (A Wartime·Peacetime OMS/MP Analysis Model for a Naval Ship and Case Study)

  • 하성철;국정호
    • 한국군사과학기술학회지
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    • 제15권5호
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    • pp.660-666
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    • 2012
  • The weapon system is getting more and more expensive, complex and smarter. Therefore, efficiently and effectively, it is important to operate the weapon system. OMS/MP is a document to quantify operational factors like as environment, mission, mode etc. It is important data to perform RAM analysis in early weapon development phase and operate better a weapon system. This paper present a process and framework of OMS/MP for a naval ship with a deep analysis of relevant domestic and abroad case studies. It propose OMS/MP analysis framework based on wartime scenario and mission area analysis. This result will contribute not only improvement for the availability of a naval ship but also enhancement of RAM analysis process.

금속-절연층-실리콘 구조에서의 비정질 GeSe 기반 Resistive Random Access Memory의 동작 특성 (Operating Characteristics of Amorphous GeSe-based Resistive Random Access Memory at Metal-Insulator-Silicon Structure)

  • 남기현;김장한;정홍배
    • 한국전기전자재료학회논문지
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    • 제29권7호
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    • pp.400-403
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    • 2016
  • The resistive memory switching characteristics of resistive random access memory (ReRAM) using the amorphous GeSe thin film have been demonstrated at Al/Ti/GeSe/$n^+$ poly Si structure. This ReRAM indicated bipolar resistive memory switching characteristics. The generation and the recombination of chalcogen cations and anions were suitable to explain the bipolar switching operation. Space charge limited current (SCLC) model and Poole-Frenkel emission is applied to explain the formation of conductive filament in the amorphous GeSe thin film. The results showed characteristics of stable switching and excellent reliability. Through the annealing condition of $400^{\circ}C$, the possibility of low temperature process was established. Very low operation current level (set current: ~ ${\mu}A$, reset current: ~ nA) was showed the possibility of low power consumption. Particularly, $n^+$ poly Si based GeSe ReRAM could be applied directly to thin film transistor (TFT).