• International Journal of Highway Engineering
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• v.8 no.4 s.30
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• pp.75-85
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• 2006

Plate Bearing Test(PBT) and California Bearing Ratio Test(CBR) usually have been used to evaluate the bearing capacity of sub-layer in pavement system. However, these tests have shortcomings for which man powers and time are spent greatly. Many researchers proposed a simple Dynamic Cone Penetrometer Test(DCP) to evaluate the bearing capacity of sub-layers in pavement system. This study performed several field bearing capacity tests(DCP, PBT, CBR, FWD) to evaluate field performance of DCP on sub-base and subgrade at four test sections simultaneously. The results showed that DCPI, $M_{FWD}$, and $PBT_K_{30}$ are highly correlated, but CBR and other test are not. This study proposed the following regression models between FWD, DCP, and PBT: $$M_{FWD}=993.10\Big(\frac{1}{DCPI}\Big)+33.95\;R^2=0.77$$ $$M_{FWD}=3.7533K_{30}+23.085\;R^2=0.69$$

• Journal of the Korean Society of Propulsion Engineers
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• v.10 no.2
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• pp.39-45
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• 2006

In liquid rocket engine turbopump, it is difficult to evaluate turbine performance for high pressure, high temperature circumstance. Turbine test is often done by using air at similarity condition so that the turbine can be tested at lower risk. This paper describes an air similarity test program of liquid rocket engine turbopump turbine. A test facility has been built to evaluate aerodynamic performance of turbines. The test facility consists of high pressure air supply system, mass flow rate measuring nozzle, test section, hydraulic break, exit orifice for pressure control, instrumentation and control system. This paper also presents how to decide the similarity conditions of the turbine test and describes how to control test conditions. Relative standard deviation of measurement parameter was less than 1% and measured turbine efficiency corresponded with analysis result within 2%.

• The Transactions of the Korea Information Processing Society
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• v.4 no.11
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• pp.2832-2839
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• 1997

In this paper, a testing architecture and procedure that an idle ATM virtual channel can be utilized for TCP channel is proposed. Four kinds or methodologies for protocol conformance testing have been standardized in ISO. Remote testing method used popularly have some disadvantages that developer must operate system manually in case of System Under Test (SUT) active testing and we cannot control and observe Implementation Under Test (IUT) often. It is proper to adopt distribute testing method than remote test in order to maximize test coverage and optimize fault coverage for conformance testing in ATM systems, and it is required that TCP channel is prepared for distribute testing method. The proposed architecture can adopt distributed testing method without extra physical channel for testing control. Also we can maximize the test coverage and implement the automation of testing without intervention of operator sustaining normal operation of ATM equipment.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.20 no.4
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• pp.479-488
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• 2019

The flight test operational procedure artifact includes mission planning, execution methods, and safety measures for each step of test progress. As the development of guided missiles has become more advanced and strategic, flight test has become increasingly complex and broadened. Therefore, increased reliability of the flight test operation procedures was required to ensure test safety. Particularly, the design of the flight test operational procedures required verification through M&S to predict and prepare for the uncertainty in a new test. The relevant studies have published the optimal framework development for flight tests and the model-based improvements of flight test processes, but they lacked the specificity to be applied directly to the flight test operational procedures. In addition, the flight test operational procedures, which consist of document bases, have caused problems such as limitations of analysis capabilities, insensitive expressions, and lack of scalability for the behavior and performance analysis of test resources. To improve these problems, this paper proposes how to design operational procedure of guided missile flight test system by applying MBSE(Model-based Systems Engineering). This research has improved reliability by increasing the ability to analyze the behavior and performance of test resources, and increased efficiency with the scalability applicable to multiple flight tests. That can be also used continuously for the guided missile flight tests that will be developed in the future.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.48 no.3
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• pp.195-205
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• 2020

This study addresses analysis on reactions which are induced in restraint system for airframe full-scale static structural test. This system restraints 6 degrees of freedom of a test article. It is valuable to study evaluating test error through analysis on the reactions which include all errors in a test. It is required to calculate fistly right reactions for the evaluation. This study focuses on calculation of the right reactions. The reaction is represented by sum of nominal reaction(Rn) and testing error reactions(Rce, Rerr) and is analyzed by two steps (inital vs relative reaction) in this study. It would evaluate intrinsic error at 0%DLL and error induced from applying test load, separately. Based on analysis using test data of a full-scale static test(canard type aircraft), resultant force of Rces and Rce_rs are distributed within 82.8N while resultant force of Rerr_rs shows to increase upto max. 808N as load level increment. Such well distribution of the Rce within the small range is caused from TMF values characteristics which are well distributed within -30N~40N. Additionally, it is shown through qualitative analysis on three components(X0, Y0, Z0) of the relative reaction(Rerr_r) that the reactions must be calculated with considering deformation of test article to calculate correctly reactions. This study shows also that equations characterizing deformation of components of test article are required to calculate the correct reactions, the equations must include information which will be used to calculate movement of all loading points.

• Journal of the Institute of Electronics and Information Engineers
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• v.53 no.11
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• pp.130-138
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• 2016

In this paper present the real-time system parallel testing techniques for weapon systems error verification. Previously field testing equipment in the military field was using the sequential testing method to maintain. This method could not check the error verification of interference. For this reason, in this paper propose the real-time system parallel testing techniques using an embedded module instead of the sequential testing techniques which is used in the weapon system error verification. Using the embedded module mounted switching control card conduct the parallel testing and then send the result to the PC. This method is possible to increase the reliability in the weapon system error verification.

• Aerospace Engineering and Technology
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• v.2 no.2
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• pp.11-17
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• 2003

This paper present a method of meter-out flow control for overload protection valve in full-scale airframe test. Emergency stop, which results in dump state, can be happened during full-scale airframe test by several causes. Because servo valve can't control hydraulics actuator in the dump state, pressure in cylinder chamber may rise abruptly and overload can be acted to the test article. In this paper, the procedure and technology of orifice setting are investigated to protect the test article from unexpected loads by dump. The test results show that the presented methods decrease peak loads and improve unloading characteristics of hydraulic actuators in the dump state.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.7 no.4
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• pp.805-811
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• 2003

System test is an important factor in the development process of good quality complex software in time, ensuring user requirements. Transaction processing module of database management systems schedules multiple transactions effectively and ensures that each transaction preserves data consistency. In this paper, we propose automatic functional testing techniques which ensure systematically that the implemented concurrency control function confirms to its requirements. The proposed testing technique tests functions of concurrency control module based on scenario without user intervention, and displays the result of functional testing. Finally, we utilize the proposed functional testing technique in the testing process of a database management system.

• Information and Communications Magazine
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• v.31 no.7
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• pp.15-23
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• 2014

"HTML5 기반 스마트 TV 플랫폼" 표준은 TV 제조사와 플랫폼 사업자 중심으로 파편화된 스마트 TV 앱 생태계 한계를 극복하고 표준 기반의 공통 플랫폼 기술을 통해 앱 생태계를 활성화 촉진시키기 위해 제정된 개방형 TV 플랫폼 기술 표준이다. 본 고에서는 이 표준 기술을 소개하고자 하며 이를 위하여 표준에 정의된 HTML5 기반의 앱 실행환경, TV 디바이스 환경을 고려한 앱 모델, 채널 프로그램과 같은 방송 자원을 접근하기 위한 인터페이스, 앱 스토어를 통한 앱 다운로드 및 실행을 위한 패키징 규칙, 멀티스크린 적응형 스트리밍 등 다양한 스마트 TV 플랫폼 관련 기술들을 설명한다. 또한, 스마트 TV 앱이 표준 기반으로 개발된 다양한 수신기에 동일하게 실행됨을 보장하기 위해 수신기에 대한 표준 구현 적합성 검증이 필요함을 제기하면서, 이를 위한 시험 기준을 정의한 "HTML5 기반 스마트 TV 플랫폼 수신기 적합성 시험" 표준에 대해서도 소개한다. 이 표준은 수신기 기능 검증을 위한 테스트 케이스를 정의하고 시험 절차 및 판정 기준 등을 규정한다. 마지막으로, 본 고는 TTA에서 실제로 이 시험 표준을 기반으로 구축한 적합성 시험 환경을 소개한다. 수신기의 표준 기술 검증용으로 시험표준에 따라 개발된 테스트 케이스와 이를 실행하고 그 결과를 수집 관리하기 위해서 구성한 웹 서버, 방송 송출 서버, 적합성 시험 관리 시스템 등의 환경 구성 요소 및 그 인터페이스에 대해서 설명한다.

• Proceedings of the Korean Geotechical Society Conference
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• 2010.03a
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• pp.951-956
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• 2010

본 연구에서는 $\bigcirc\bigcirc$화력발전소 회사장에 매립되고 있는 혼합회가 도로성토 및 철도노반 등 성토재로 사용될 수 있는가를 평가하기 위하여 물리적 및 역학적 특성을 평가하였다. 비중, 액소성 시험, 입도분석, XRD 시험, 강열감량시험, 실내투수시험을 통해 물리적 특성을 평가하였고 다짐시험, CBR 시험, 배수삼축압축시험을 실시하여 역학적 특성을 평가하였다. 두 가지 혼합회에 실험한 결과 비중은 2.181~2.189, 투수계수는 $1.32{\times}10^{-4}{\sim}1.89{\times}10^{-4}cm/sec$, 수정CBR은 19.5~21%, 배수마찰각은 $36.43{\sim}41.39^{\circ}$로 평가 되었다. 혼합회의 투수계수는 실트질 흙과 유사한 범위에 있으며 배수마찰각은 상대밀도가 큰 모래질 흙이 보일 수 있는 내부마찰각의 범위를 보였다. 본 연구에서 사용한 혼합회는 도로성토 및 철도노반 등 성토재로 사용할 수 있는 것으로 평가되었다.