• Proceedings of the Korean Information Science Society Conference
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• 2001.04a
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• pp.745-747
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• 2001

인터넷 망을 통한 멀티미디어 컨텐츠 서비스는 다른 종류의 서비스와 달리 제 사간에 연속적으로 재생되어야 의미를 갖는 데이터들로 이루어져있으며, 이러한 속성을 얼마나 충족시키느냐에 따라 QoS가 결정된다. 좋은 서비스를 제공하기 위하여 원래서브의 부본서버를 여러 개 두어 서비스 요청을 분산시키는 방법을 많이 사용하고 있다. 본 연구에서는 클라이언트의 요청에 능동적으로 그리고 효과적으로 서비스하도록 웹로그 문서전송 서비스양의 분포에 따른 사전정보를 가지고 각 부본서버의 부하량을 체크하고, 이후에 발생하는 클라이어트의 요청을 분산시킬 수 있는 동적 알고리즘을 재안한다. 본 동적선택 알고리즘은 QoS가 중요한 대량의 멀티미디어 컨텐츠를 전송함에 있어서 HTTP 반응시간과 문서크기의 변동에 따른 근접척도 공정능력지수를 이용하여 클라이어트 요청을 확률분산시키는 것이다.

• Proceedings of the Korea Information Processing Society Conference
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• 2002.04b
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• pp.1503-1506
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• 2002

현재, 네트워크는 컴퓨터 환경의 급속한 발달과 함께 빠른 속도로 확장되고 있다. 그러면서 거대한 인터넷의 경계도 끝없이 확장되고 있다. 인터넷은 네트워크의 네트워크라고 일컬어진다. 즉, 인터넷은 사설 혹은 공용 네트워크로 이루어진 연결된 하나의 거대한 네트워크이다. 하지만 이러한 네트워크를 이용하기 위해서는 전체 인터넷에 연결되기 위한 공통된 약속된 주소를 가져야만 한다. 그러므로 전 세계의 모든 호스트를 연결하는 데는 물리적 한계가 있으며 현재 인터넷 주소체계의 한계가 나타나기 시작했다. 진정한 의미의 인터넷은 네트워크의 무한한 확장에 있다고 생각했을 때 현재의 방식은 인터넷의 진정한 의미에 부합하지 못한다. 본 논문에서는 IP의 공유를 통한 현재의 네트워크의 효율성 제고 및 서브 네트워크에서의 서버 구축이 네트워크의 개선을 이룰 수 있음을 증명한다. 그리고 TCP/IP 기반의 인트라넷 통신의 확장, 이에 따른 네트워크 토폴로지를 제시해 단일회선 이하에서 네트워크를 구현하고 이의 이용에 관해 제시한다.

• Proceedings of the Korean Information Science Society Conference
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• 1999.10a
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• pp.584-586
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• 1999

소프트웨어 개발 시 기존 전문가들의 개발 경험을 재사용하는 작업은 개발 기간의 단축 및 비용의 절감의 효과를 가져올 수 있다. 이러한 재사용에 관련된 연구는 소프트웨어공학 분야에서 계속되어 그 하나로 객체지향 프레임워크를 들 수 있다. 객체지향 프레임워크는 검증된 소프트웨어 재사용 부품으로 특정 도메인에 대한 비즈니스 로직을 재사용할 수 있도록 구현된다. 프레임워크 내부에는 재사용되는 로직이 포함되어 있으며 프레임워크 사용자에 의해 커스터마이징 될 모듈을 정의하고 있다. 프레임워크 사용자는 프레임워크를 기반으로 어플리케이션을 개발함으로써 처음부터 개발을 시작하지 않으며 기 개발자들의 경험을 재사용하게 된다. 본 논문에서는 근래 크게 대두되고 있는 가상상점 도메인에 대한 프레임워크를 제시한다. 본 논문에서 제시하는 가사상점 프레임워크는 제인 프레임워크와 주문, 지불, 배달의 3개 서브프레임워크로 구성되며 각각의 프레임워크가 포함한 핫스팟, 제어흐름, 프레임워크 인터페이스를 중심으로 프레임워크의 구성요소 및 설계, 구현에 관한 사항을 기술한다.

• Korean Chemical Engineering Research
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• v.54 no.3
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• pp.360-366
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• 2016

The Propulsion Test Facilities for the development of Korea Space Launch Vehicle-II are being built, some test facilities are completed and various combustion tests are running. The Propulsion Test Facilities consists test-stand, which carries out tests for engine development model, and various sub-systems and vessels containing LOX and Jet A-1 as propellant. There are always risks of fire and explosion at the test-stand since engine development model is conducted at test-stand with real combustion test with very high pressure, mixed propellant and high energy. In this paper, in order to establish the consequence analysis and risk reduction measures in the Propulsion Test Facilities, followings are considered. 1) a propellant leak accident scenario is assumed in test-stand. 2) TNT equivalent model equation based on blast wave of the explosion was used to analyze blast overpressure and impacts. Also, technical, systematic and managemental measure is described to ensure risk reduction for propulsion test facility.

• Journal of the Korean Society of Propulsion Engineers
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• v.18 no.1
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• pp.91-96
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• 2014

KSLV-I (Korea Space Launch Vehicle-I) upper stage KM (Kick Motor) is a solid propulsion system which consists of igniter, SAD (Safety Arming Device), composite case, and submerged nozzle capable of TVC (Thrust Vector Control) actuation. Each subsystem of KM fulfilled development requirements for achieving a flight mission successfully. We confirmed the successful development of KM from the $3^{rd}$ flight test results of NARO on January 30, 2013. This article deals with the requirements of KM and the results on configuration management, mass variation, thrust axis alignment, and major test results and so on.

• Journal of the Korea institute for structural maintenance and inspection
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• v.12 no.5
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• pp.169-178
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• 2008

Compressive flanges of steel box girder is designed based on the ultimate strength behavior of sub-panel which is enclosed with longitudinal stiffeners and transverse stiffeners on appropriate safety factor. However, it is rational that the ultimate strength is calculated considering the various factors such as number and stiffness of longitudinal stiffener, spacing of transverse stiffener, initial deformation and residual stress distribution. In this study, an analysis program based on Folded Plate theory is developed considering the geometric effects and the material nonlinearity. The analysis program is applicated to the steel box girder bridges which is really constructed in domestic.

• Journal of the Korean Society of Propulsion Engineers
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• v.13 no.3
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• pp.20-26
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• 2009

Turbopump test for a 30-ton-thrust liquid rocket engine was carried out using real-propellant. Liquid oxygen, kerosene, cold hydrogen gas were used for the oxidizer pump, the fuel pump, and the turbine, respectively. The turbopump was reliably operated at the design and off-design conditions and the performance requirements were satisfied, which implies that the turbopump development at the engine subsystem level is successfully accomplished in the point of performance validation. This paper presents the results of a test where the turbopump was run for 75 seconds at three operating modes. In terms of performance characteristics of pumps and turbine, the results of turbopump assembly test using real-propellant showed a good agreement with those of the turbopump component tests using simulant working fluid.

• Journal of the Institute of Electronics Engineers of Korea SP
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• v.38 no.2
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• pp.179-190
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• 2001

In this proposed study, observing and analyzing contrast enhanced abdominal CT images, we segmented the liver automatically. We computed the ratio of each gray value from the estimated gray value range. With the average value of mesh image, we distinguished the liver from the noise parts. We divided the region based on immersion simulation. The threshold value is determined from the mesh image which is generated from each gray value portion of the liver and is used in dividing the liver to the noise region. To get the outline of the liver, we generated template image which represents the lump of the liver, and subtracted it from the binary image. With the results we use the proposed algorithm using 8-connectivity instead of the present opening algorithm, to reduce the processing time. We computed the volume from the segmented organ size and presented a clinical demonstration with the animal experiment

• Journal of the Korean Society of Propulsion Engineers
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• v.19 no.4
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• pp.85-93
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• 2015

Liquid rocket engines of KSLV-II employ a turbopump feed system for propellants. A turbopump real-propellant test facility based on liquid oxygen and kerosene has been constructed for the experimental verification of the turbopump performance using the real media of propellants(i.e., LOX/Kerosene). The verification tests of sub-systems were performed such as LOX/kerosene feed system and alcohol burner system. Finally, the performance of the whole system was executed and verified through a sets of validation tests with the development model of the KSLV-II turbopumps. It has been confirmed that the test facility satisfies the operating conditions and time of the turbopump at the design and off-design performance test using real-propellant.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.11a
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• pp.892-897
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• 2011

The propulsion system of space launch vehicle generates thrust by supplying oxidizer and fuel to combustion chamber. KSLV-II 2nd stage engine, currently under development by KARI, is to use liquid oxygen as a oxidizer and JET-A1 as a fuel. The 2nd stage pump-fed engine is mainly composed of combustion chamber, turbo-pump and engine supply system. To develop liquid propulsion engine, the development of combustion chamber must be preceded. For performance validation of the combustion chamber, the designed and manufactured combustion chamber should be tested in combustion chamber test facility(CCTF). The detailed design for the planned CCTF in Naro Space Center was conducted. The fuel supply system modeling using AMESim was performed based on the results of the detailed design, and the fuel supply characteristics was analyzed in this paper.