• 한국정보과학회논문지:시스템및이론
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• 제36권3호
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• pp.171-180
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• 2009

바이트 단위 임의 접근이라는 램 특성과, 비휘발성이라는 디스크의 특성을 동시에 제공하는 FeRAM, MRAM, PRAM등의 스토리지 클래스 램(Storage Class Random Access Memory, SCRAM)이 소형 임베디드 시스템을 중심으로 점차 그 활용범위를 넓혀가고 있다. 본 논문에서는 SCRAM을 주기억 장치 및 보조 기억 장치로서 동시에 사용할 수 있는 차세대 통합 소프트웨어 구조를 제안한다. 제안된 구조는 크게 스토리지 클래스 램 드라이버(SCRAM Driver)와 스토리지 클래스 램 관리자(SCRAM Manager)로 구성된다. SCRAM Driver는 SCRAM을 직접 관리하며, FAT이나 Ext2와 같은 전통적인 파일 시스템이나 버디 할당자와 같은 전통적인 메모리 관리자, 혹은 SCRAM Manager 등의 상위 소프트웨어 계층에 저수준 인터페이스를 제공한다. SCRAM Manager는 파일 객체와 메모리 객체를 통합하여 관리함으로써 이들 간에 부가적인 비용이 없는 변환을 가능케 한다. 제안된 기법은 FeRAM이 장착된 실제 시스템에서 실험되었으며, 실험 결과를 통해 SCRAM Driver가 효율적으로 전통적인 파일시스템과 메모리 관리자가 요구하는 기능을 제공할 수 있음을 보였다. 또한 기존의 파일 시스템과 메모리 관리자를 통해 각각 SCRAM을 접하는 경우보다 SCRAM Manager가 수십 배 빠른 성능을 보임을 확인할 수 있었다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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• pp.85-92
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• 2004

As a research to develop a SCRAM jet engine is actively conducted, a necessity to produce a high-enthalpy flow in a laboratory is increasing. In order to develop the SCRAM-jet engine, stabilized combustion in a supersonic flow-field should be attained, in which a duration time of flow is extremely short. Therefore, a mixing process of breathed air and fuel, which is injected into supersonic flow-fields is one of the most important problem. Since, the flow inside SCRAM jet engine has high-enthalpy, an experimental facility is required to produce such high-enthalpy flow-field. In this study, a detonation-driven shock tunnel was built and was used to produce high-enthalpy flow. Further-more, SCRAM jet engine model equipped backward-facing step was installed at test section and flow-fields were visualized using color-schlieren technique and high speed video camera. The fuel was injected perpendicular to the flow of Mach number three behind backward-facing step. The height of the step, distance of injection and injection pressure were changed to investigate the effects of step on a mixing characteristic between air and fuel. The schlieren photograph and pressure histories show that the fuel was ignited behind the step.

• 정보과학회지
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• 제27권5호
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• pp.29-37
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• 2009

• 한국유체기계학회 논문집
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• 제18권6호
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• pp.5-11
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• 2015

In a pressurized water reactor (PWR), control rod assembly (CRA) falls into the guide tubes of a fuel assembly due to gravity for scram. Various theoretical approaches and numerical analyses have been performed because its shape is simple and its design was completely developed several decades ago. A control rod assembly for a sodium-cooled faster reactor (SFR) which is geometrically more complicated is being actively developed in Korea nowadays. Drop time and impact velocity of a CRA are important parameters with respect to reactivity insertion time and the mechanical robustness of a CRA and a guide duct. In this paper, computational method considering simultaneously the equation of motion for rigid body and the Navier-Stokes equations for fluid is suggested and verified by comparison with theoretical analysis results. Through this valuable CFD analysis method, drop time and impact velocity of initially designed SFR CRA are evaluated before performing scram tests with it.

• 한국원자력학회:학술대회논문집
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• 한국원자력학회 2003년도 춘계학술발표대회 요약집
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• pp.179-179
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• 2003

• 한국원자력학회:학술대회논문집
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• 한국원자력학회 2002년도 춘계공동학술발표회요약집
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• pp.164-164
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• 2002

• 한국연소학회지
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• 제1권1호
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• pp.83-91
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• 1996

A numerical study is carried out to examine the ignition and propagation process of detonation wave in SCRam-accelerator operating in superdetonative mode. The time accurate solution of Reynolds averaged Navier-Stokes equations for chemically reacting flow is obtained by using the fully implicit numerical method and the higher order upwind scheme. As a result, it is clarified that the ignition process has its origin to the hot temperature region caused by shock-boundary layer interaction at the shoulder of projectile. After the ignition, the oblique detonation wave is generated and propagates toward the inlet while constructing complex shock-shock interaction and shock-boundary layer interaction. Finally, a standing oblique detonation wave is formed at the conical ramp.

• Nuclear Engineering and Technology
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• 제15권1호
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• pp.50-56
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• 1983

Scram이 일어난 후 과도 기간 동안 LMFBR 출구공간에 있어서의 유동성층의 영향은 특별한 문제로 제기되고 있다. 이러한 경우에 난류 혼합에 미치는 부력 효과는 설계자에게 중요하다. 난류 유동 방정식에 부력 효과를 갖지 않는 기존 난류 모형의 부력효과를 더하기 위한 연구가 행해졌다. 개발된 부력 난류 유동의 물리적 모형은 SMAC 수치 해석 방법을 통하여 풀어졌다. 개발된 수치 해석 모형이 시험되어졌고, 실험자료와도 비교되었다. 결과는 난류에 대한 부력 효과가 출구공간에서 난류를 강하게 억압하며 성층의 안정도를 상당히 증가시켰다.

• Nuclear Engineering and Technology
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• 제36권6호
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• pp.485-496
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• 2004

Typical probabilistic safety assessment (PSA) results were used to estimate the performance indicator (PI) thresholds of unplanned reactor scram (URS) and safety system unavailability (SSU) for Korean nuclear power plants (NPPs). The changes in core damage frequency (${\Delta}$CDFs) of $10^{-6}/yr$, $10^{-5}/yr$, and $10^{-4}/yr$ were adopted as the risk criteria in setting up the PI thresholds. The PI thresholds for the URS were estimated using information pertaining to the initiating event frequencies, the CDF, and the CDF contribution of each initiating event. The PI thresholds of the SSU were estimated using information on the unavailability, the Fussell-Vesely importance, and the CDF.

• 한국지진공학회:학술대회논문집
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• 한국지진공학회 2006년도 학술발표회 논문집
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• pp.563-570
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• 2006

Distributed control architecture is based on sharing control and data between multiple nodes on a network Communication and task sharing can be distributed between multiple control computers. Although many communication protocols exist, such as TCP/IP and UDP, they do not have the determinism that realtime control demands. Fiber-optic reflective shared memory creates the opportunity for realtime distributed control. This architecture allows control and computational tasks to be divided between multiple systems and operate in a deterministic realtime environment. One such shared memory architecture is based on Curtiss-Wright ScramNET family of fiber-optic reflective memory. MTS has built seismic and structural control software and hardware capable of utilizing ScramNET shared memory, opening up infinite possibilities in research and new capabilities in Hybrid and Model-In-The-Loop control.