• 한국인터넷방송통신학회논문지
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• 제22권6호
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• pp.149-154
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• 2022

GaN 소자는 고출력 및 고선형성 특성을 가지므로 레이더 수신기에서 저잡음 증폭기로 활용되어 리미터 없이 구현될 수 있으며, 이로 인해 잡음지수를 개선하고 면적을 줄일 수 있다. 본 논문에서는 Ka-대역 레이더용 수신기에 적용하기 위한 GaN 저잡음 증폭기를 기술하였다. 설계된 저잡음 증폭기는 150-nm GaN HEMT 공정으로 제작되었으며, 목표주파수 내에서 패키징 손실을 포함하여 >23 dB 이득, <6.5 dB의 잡음지수 특성을 보였다. 고입력 부하시험시 이득 및 잡음 저하가 있었으나, 반복시험시 추가적인 성능저하는 나타나지 않았다. 부하시험 후 잡음지수 및 S-파라미터 측정을 통해 GaN 저잡음 증폭기에서 ~40 dBm 펄스 입력 전력을 견딜 수 있음을 확인하였다.

• 융합보안논문지
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• 제21권1호
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• pp.177-189
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• 2021

국방 연구개발은 변화하는 미래 전장환경에 대응하기 위해 중·장기 소요로 결정된 무기체계를 확보하기 위한 핵심과정이다. 특히 시험평가는 무기체계 연구개발의 마지막 관문으로서 전력화 전환여부를 결정하는데 필요한 정보를 제공해주고 무기체계의 수명주기와 연계된 성능보장을 위해서도 중요한 역할을 수행한다. 한편 최근 한반도 작전환경 및 국방 획득환경의 변화를 살펴보면, 크게 3가지 특징을 확인할 수 있다. 먼저 무기체계 전력화 운용시 지속적인 안전사고가 발생하여 전투원 안전에 대한 사회적 관심이 증대되었고, 획득비용의 증가에 따라 한정된 국방예산의 효율적 집행이 요구되고 있다. 또한 로봇·자율무기체계(RAS), 사이버 보안 시험평가 등 미래 전장환경에 대응하기 위한 전략적 접근이 필요하다. 따라서 본 연구에서는 최근 변화된 안보환경의 특징을 고찰하여 무기체계 운용시험평가의 개선전략을 제시하고자 한다. 이를 위해 현행 무기체계 운용시험평가 시스템의 보완소요를 다차원 모형으로 분석하여 개선전략을 도출하였고 계층적 분석기법(AHP)을 통해 우선순위를 결정하였다.

• 한국군사과학기술학회지
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• 제27권1호
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• pp.24-30
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• 2024

The gas-gun test is a experimental approach employed to validate the operational or structural stability when subjected to the impact energy encountered during launch or target collision. Predicting the outcomes of the gas-gun test has traditionally relied on empirical knowledge, due to numerous factors such as the bird assembly's shape, weight, material, and flight velocity. However, due to the nonlinearity and complex interactions between these variables, numerous tests are necessary to identify the necessary requirements, resulting in significant expense and time consumption during the process. The objective of this study is to forecast the variations in impact energy in future tests by developing a numerical model and analysis that aligns with the test outcomes, utilizing the ABAQUS Explicit. The outcome of the numerical analysis produced a framework that anticipates the peak g and the duration of the actual gas-sun test results, throughout post-processing techniques using FFT and LPF filters.

• Corrosion Science and Technology
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• 제14권3호
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• pp.120-126
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• 2015

The usage of bending products recently have increased since many industries such as automobile, aerospace, shipbuilding, and chemical plants need the application of pipings. Bending process is one of the inevitable steps to fabricate the facilities. Induction heat bending is composed of compressive bending process by local heating and cooling. This work focused on the effect of induction heat bending process on the properties of ASME SA312 Gr. TP304 stainless steel pipes. Tests were performed for base metal and bended area including extrados, intrados, crown up, and down parts. Microstructure was analyzed using an optical microscope and SEM. In order to determine intergranular corrosion resistance, Double Loop Electrochemical Potentiokinetic Reactivation (DL-EPR) test and ASTM A262 practice A and C tests were done. Every specimen revealed non-metallic inclusion free under the criteria of 1.5i of the standard and the induction heat bending process did not affect the non-metallic inclusion in the alloys. Also, all the bended specimens had finer grain size than ASTM grain size number 5 corresponding to the grain sizes of the base metal and thus the grain size of the pipe bended by induction heat bending process is acceptable. Hardness of transition start, bend, and transition end areas of ASME SA312 TP304 stainless steel was a little higher than that of base metal. Intergranular corrosion behavior was determined by ASTM A262 practice A and C and DL-EPR test, and respectively step structure, corrosion rate under 0.3 mm/y, and Degree of Sensitization (DOS) of 0.001~0.075% were obtained. That is, the induction heat bending process didn't affect the intergranular corrosion behavior of ASME SA312 TP304 stainless steel.

• 한국항공우주학회지
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• 제45권4호
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• pp.269-275
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• 2017

전투기 형태의 항공기는 외부 장착물의 중량, 공력 특성 및 조합 형태에 따라 공력탄성학적 특성에 상당한 영향을 받게 된다. 따라서 항공기를 운용하기에 앞서 기본적으로 모든 외부 장착물 조합에 대한 공력탄성학적 안정성이 반드시 검증되어야 한다. 그러나 공력탄성학적 안정성을 분석하기 위해서는 항공기의 구조, 중량, 조종면 특성, 외부형상 등과 같은 설계 데이터가 필요함에 따라, 원칙적으로 항공기 플랫폼을 개발한 제작사 이외에는 적합성 입증을 수행하는데 상당한 제한이 따를 수밖에 없다. 그럼에도 불구하고 작전환경의 변화 및 항전기술의 발전으로 인해 원 제작사의 지원 없이 항공기를 운용하는 국가 또는 기관에서 자체적으로 신규 장착물을 장착해야 하는 상황이 있을 수 있다. 본 논문에서는 이와 같이 설계 데이터를 갖고 있지 않은 도입 항공기에 대해 신규 장착물을 장착하는데 필요한 공력탄성학적 적합성 입증 방안에 대해 기술하였다.

• 마이크로전자및패키징학회지
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• 제26권3호
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• pp.43-49
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• 2019

본 연구에서는 그래핀 산화(graphene oxide, GO) 분말 복합 Sn-3.0Ag-0.5Cu(in wt.%) 솔더페이스트를 이용한 플렉시블 기판과 SOP(small outline package) 사이의 솔더 접합부의 굽힘 신뢰성 향상에 관한 새로운 접근을 제안하였다. 솔더페이스트에 GO의 첨가는 녹는점에 약간의 영향을 미치었으나 그 차이는 미미한 것으로 나타났다. 한편, GO의 첨가는 리플로우 공정 동안 솔더 접합부의 금속간화합물(intermetallic compound, IMC) 성장과 두께를 억제 할 수 있음을 확인하였다. 더욱이 접합부의 신뢰성에 미치는 영향을 살펴보고자 반복 굽힘 시험을 진행하였으며 GO 분말의 첨가로 솔더 접합부의 반복 굽힘 신뢰성 향상 시킬 수 있었다. 0.2 wt.%의 GO가 첨가된 솔더 접합부의 경우 GO가 첨가되지 않은 경우에 비하여 굽힘 수명은 20% 가량 증가하는 것으로 나타났다. GO가 첨가된 경우 솔더 접합부의 인장 강도와 연성이 증가하게 나타났는데 이러한 GO 첨가에 의한 기계적 특성 향상이 솔더 접합부의 반복 굽힘 신뢰성 향상에 기여한 것으로 추측된다.

• 대한의용생체공학회:의공학회지
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• 제40권5호
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• pp.197-205
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• 2019

The existing Extracorporeal membrane oxygenation(ECMO) and Cardiopulmonary bypass system(CPB) have been developed and applied to various devices according to their respective indications. However, due to the complicated configuration and difficult usage method, it causes inconvenience to users and there is a risk of an accident. Therefore, smart all-in-one cardiopulmonary circulation device is being developed recently. The smart all-in-one cardiopulmonary assist device consists of a blood pump for cardiopulmonary bypass, a blood oxidizer for cardiopulmonary bypass, a blood circuit for cardiopulmonary bypass, and an artificial cardiopulmonary device. It is an integrated cardiopulmonary bypass device that can be used for a variety of purposes such as emergency, intraoperative, post-operative intensive care, and long-term cardiopulmonary assist, combined with CPB used in open heart surgery and ECMO used when patient's cardiopulmonary function does not work normally. The smart all-in-one cardiopulmonary assist device does not exist as a standard and international standard applicable to advanced medical devices. Therefore, in this study, we will refer to the International Standard for Blood Components, the International Standard for Blood, the Guideline for Blood Products, and prepare applicable performance and safety guidelines to help quality control of medical devices, and contribute to the improvement of the health of people. The guideline, which is the result of conducted a survey of the method of safety and performance test, is based on the principle of all-in-one cardiopulmonary aiding device, related domestic foreign standards, the status of domestic and foreign patents, related literature, blood pump(ISO 18242), blood oxygenator (ISO 7199), and blood circuit (ISO 15676) for cardiopulmonary bypass.The items on blood safety are as follows: American Society for Testing and Materials ASTM F1841-97R17), and in the 2010 Food and Drug Administration's Safety Assessment Guidelines for Medical Assisted Circulatory Devices. In addition, after reviewing the guidelines drawn up through expert consultation bodies including manufacturers / importers, testing inspectors, academia, etc. the final guideline was established through revision and supplementation process. Therefore, we propose guidelines for evaluating the safety and performance of smart all-in-one cardiopulmonary assist devices in line with growing technology.

• Educational Technology International
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• 제25권1호
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• pp.93-127
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• 2024

This study evaluates the effect of structured debriefing for a business simulation game for university students. The program provides an authentic learning experience of real-world business management by allowing learners to make decisions related to R&D, marketing, production, and finance through a business simulation game, and check the results in real time. In 2022, University A and B each ran a business simulation game-based program as an extra-curricular activity. University A conducted a traditional instructor-led debriefing where the instructor explained the summarized process and results, while University B implemented a structured debriefing which had been developed based on Gibbs' and 3D models. To assess the effect of the structured debriefing compared to the traditional instructor-led debriefing, business knowledge and entrepreneurship competencies were measured three times. Repeated measures ANOVA was used to test for the differences between the two groups and to examine interaction effects between group and time. The structured debriefing group achieved statistically significantly higher academic scores than the traditional instructor-led debriefing group at the post-test and in 2 weeks. There was no statistically significant difference between the groups in terms of entrepreneurship competencies. There was no interaction effect between group and time, both in academic achievement and in entrepreneurship competencies. In conclusion, the simulation game-based program integrated with the structured debriefing session is more likely to have a stronger impact on academic achievement and its retention.

• Steel and Composite Structures
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• 제24권5호
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• pp.615-633
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• 2017

Fatigue crack initiated in welded tubular joints due to cyclic loading may produce harmful effect on the integrity of the tubular structures. To study such effect, both fatigue and static tests on nine circular tubular T-joint specimens made of carbon steel materials were carried out. The specimens were subjected to tensile loading in both fatigue and static tests. The load-displacement relation, the crack propagation and the failure mode of the specimens are all analyzed. The deterioration of the static strength of the cracked T-joints is also investigated and evaluated through an area reduction factor. Experimental results indicate that the static strength of a tubular T-joint with a surface crack seems to decrease slightly while a through crack has relatively remarkable effect on the reduction of the static strength. Additionally, experimental results also show that the toughness of the materials and the geometry of the specimens play an important role on the failure process of cracked tubular T-joints.

• 한국자동차공학회논문집
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• 제18권4호
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• pp.121-126
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• 2010

The automotive weather strip has functions of isolating of water, dust, noise and vibration from outside. To achieve good sealing performance, weather strip should be designed to have the high contact force and wide contact area. However, these design causes excessive permanent deformation of weather strip. The causes of permanent deformation is generally explained to be the chemical material detrioration and physical variation and cyclic loading, etc. This paper introduces a numerical method to predict the permanent deformation using the time dependent viscoelastic model which is represented by Prony series in ABAQUS. Uniaxial tension and creep tests were conducted to obtain the material data. And the lab. test for the permanent deformation was accelerated during shorter time, 300 hours. The permanent deformation of weather strip was successfully predicted under the different loading conditions and different section shapes using the suggested numerical process.