• 한국항공우주학회지
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• 제48권7호
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• pp.489-495
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• 2020

충격파 터널에서 항력 측정을 위하여 가속도계 기반 시스템을 설계 및 구축하고, 마하 6 유동조건에서 원뿔형 모델의 항력계수를 측정하였다. 항력 측정 시스템의 마찰력을 보정하기 위하여 간단하고 직관적인 교정 방식을 제시하고, 항력 측정 결과를 단순 원뿔형 모델의 전산유체역학 해석 결과와 비교, 분석하였다. 다양한 형상의 지지대를 이용하여 지지대에 의한 항력 측정 간섭 영향을 파악하고 이를 최소화하기 위한 디자인을 제시하였다. 수정된 지지대를 이용하여 항력계수를 측정한 결과, 지지대에 의한 항력계수 오차가 작아지는 것이 확인되었다.

• 한국자동차공학회논문집
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• 제24권6호
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• pp.649-659
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• 2016

This paper describes control algorithm and control structure of vehicle control unit for range-extended electric vehicle equipped with engine-generator system, and specially presents methods which determine optimal operating points and decreases a vibration or a shock for operating the engine-generating system. The vehicle control algorithm is consisted of several parts which are sequence control, calculation of wheel demand torque, determination of operating points, and management of operating points and so vehicle controller has be made possible to efficiently manage calibration parameters. The control algorithm is evaluated by driving test modes, launching performance and operating engine-generator system and so on. In conclusion, this paper present methods for extending a mileage, improving a launching performance and reducing vibration or shock when the engine-generating system is starting or is stopping.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2011년도 추계학술대회 논문집
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• pp.370-373
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• 2011

The subcommittee 3 (SC3) of Technical Committee 108 (TC 108) covers the calibration of mechanical vibration and shock measuring pickups and instruments. This paper introduces what KS codes are linked to the ISO standards developed by TC108 / SC3. It is shown that the KS codes do not fulfill the full set of ISO codes approved in the field of TC 108/SC3. Series of ISO standards established by the Working Group 6 (WG6) of SC3 are introduced. Main objectives of those WG 6 efforts are shown to replace the old versions of ISO 5347 series into new ISO 16063 series. Their features are briefly summarized in this paper. Finally, challenging technical issues underlying behind ISO TC108 / SC3 are addressed,, such as MEMS typed linear and angular vibration pickups.

• Structural Engineering and Mechanics
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• 제32권2호
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• pp.283-300
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• 2009

The characteristic response of a structure to blast load may be divided into two distinctive phases, namely the direct blast response during which the shock wave effect and localized damage take place, and the post-blast phase whereby progressive collapse may occur. A reliable post-blast analysis depends on a sound understanding of the direct blast effect. Because of the complex loading environment and the stress wave effects, the analysis on the direct effect often necessitates a high fidelity numerical model with coupled fluid (air) and solid subdomains. In such a modelling framework, an appropriate representation of the blast load and the high nonlinearity of the material response is a key to a reliable outcome. This paper presents a series of calibration study on these two important modelling considerations in a coupled Eulerian-Lagrangian framework using a hydrocode. The calibration of the simulated blast load is carried out for both free air and internal explosions. The simulation of the extreme dynamic response of concrete components is achieved using an advanced concrete damage model in conjunction with an element erosion scheme. Validation simulations are conducted for two representative scenarios; one involves a concrete slab under internal blast, and the other with a RC column under air blast, with a particular focus on the simulation sensitivity to the mesh size and the erosion criterion.

• 오토저널
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• 제13권3호
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• pp.32-42
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• 1991

In SI engine research the pressure data in cylinder is the most important fundamental ones leading to engine efficiencies and performances. It is, therefore, necessary to obtain accurate pressure data and yet it is often impossible to install a reliable data producing, flush-mounted type pressure transducer in a cylinder of small and medium size multicylinder SI engines. When flush mounting the transducer is not possible, the spark-plug type pressure transducer is commonly used as an alternative. In this case, the transmission tube of spark-plug type pressure transducer introduces distortions in the pressure signal. Efforts were made to understand the dynamic characteristics of spark-plug pressure transducer by shock tube tests and real engine experiments. In engine experiment the cylinder pressure data were simultaneously obtained by both flush mounted and spark-plug type pressure transducers of certain transmission tube geometry. Those pressure data collected by spark-plug type pressure transducer were tested for correction to flush mounted ones by the application of transfer function. As a result of the calibration the IMEP difference between F/M data and improved S/P data was shown to be corrected about 75-98% from the original ones.

• 약학회지
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• 제58권3호
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• pp.158-164
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• 2014

Dangguisu-san is a well-known traditional Korean herbal medicine prescription and has been widely used to treat ecchymosis, blood stagnation, and pain resulting from physical shock in Korea. In this study, an ultra-performance liquid chromatography-electrospray ionization-mass spectrometer method was established for the simultaneous determination of the 17 biomarker components in Dangguisu-san. All analytes were separated on an UPLC BEH $C_{18}$ ($100{\times}2.1$ mm, $1.7{\mu}m$) column and maintained at $45^{\circ}C$. The mobile phase consisted of two solvent systems, 0.1% (v/v) formic acid in water (A) and acetonitrile (B) by gradient flow. The injection volume was $2.0{\mu}l$ and the flow rate was 0.3 ml/min with detection at mass spectrometer. Calibration curves of the 17 biomarker components were acquired with $r^2$ values ${\geq}0.9951$. The values of limit of detection and quantification of all analytes were 0.02~6.32 ng/ml and 0.05~18.95 ng/ml, respectively. The amounts of the 17 components in Dangguisu-san sample were $3.17{\sim}13,224.50{\mu}g/g$.

• 한국전자통신학회논문지
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• 제17권5호
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• pp.927-932
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• 2022

측기의 드리프트는 시간의 경과, 환경변화, 마모, 충격, 진동, 전자기장 그리고 부적절한 사용 등에 의해 발생한다. 제한된 시험 기간에 출력값의 변화를 직접적으로 드리프트로 결정하는 것은 부적절하므로 측기 교정 방법에 시간에 따른 변화를 부여하여 제로 드리프트와 스팬 드리프트를 모두 반영하는 새로운 알고리즘을 제안하였다. 승온과 감온 과정의 아홉 단계 항온 환경에서 1분 간격으로 약 60분 동안 측정한 온도의 드리프트는 0.49%로 산출되었다.

• 한국지능시스템학회논문지
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• 제20권2호
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• pp.304-310
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• 2010

현대를 살아가는 현대인들이 경험하는 만성통증 및 디스크는 성인의 80% 이상이 경험하는 흔한 질병이다. 이러한 질환들 중 교통사고, 추락 등 물리적인 충격에 의한 발생율은 10%정도이며 대부분이 습관적으로 부적합한 자세를 취하게 되어 특정 부위에 지속적인 스트레스가 쌓여 발생하게 된다. 이처럼 부적합한 자세가 오랫동안 이어져 질환의 원인이 되는 것을 알면서도 고쳐지지 않는 이유는 지속적인 반복을 통한 습관화로 인하여 부적합한 자세를 바로 인지하지 못함으로써 바르게 교정하지 못하고 지속되어지기 때문이다. 따라서 본 시스템은 자세를 측정할 수 있는 센서들을 사용자에게 부착 후 사용자의 자세에 따른 데이터를 수집하여 정확한 자세를 측정하고 자세추정알고리즘을 이용하여 해당 자세의 적합여부를 추정한다. 사용자가 부적합한 자세를 지속적으로 취할 경우 이를 인지할 수 있도록 한다. 그리고 적합한 자세로 변경하도록 유도하여 부적합한 자세의 습관화를 방지하는데 목적을 두고 있다. 또한 부적합한 자세의 원인을 분석 후 제거하여 적합한 자세를 취하는데 보조자의 기능을 수행 한다. 정확한 측정을 통한 반복적인 인지 학습을 통해 올바른 자세를 습관화 한다면 성장기 어린이와 만성 질환자에게 많은 도움을 줄 것으로 생각 된다.

• 천문학회보
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• 제41권2호
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• pp.64.3-65
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• 2016

The NISS (Near-infrared Imaging Spectrometer for Star formation history) is the near-infrared instrument optimized to the Next Generation of small satellite series (NEXTSat). The capability of both imaging and low spectral resolution spectroscopy in the near-infrared range is a unique function of the NISS. The major scientific mission is to study the cosmic star formation history in local and distant universe. For those purposes, the main observational targets are nearby galaxies, galaxy clusters, star-forming regions and low background regions. The off-axis optical design is optimized to have a wide field of view ($2deg.{\times}2deg.$) as well as the wide wavelength range from 0.95 to $3.8{\mu}m$. Two linear variable filters are used to realize the imaging spectroscopy with the spectral resolution of ~20. The mechanical structure is considered to endure the launching condition as well as the space environment. The compact dewar is confirmed to operate the infrared detector as well as filters at 80K stage. The electronics is tested to obtain and process the signal from infrared sensor and to communicate with the satellite. After the test and calibration of the engineering qualification model (EQM), the flight model of the NSS is assembled and integrated into the satellite. To verify operations of the satellite in space, the space environment tests such as the vibration, shock and thermal-vacuum test were performed. Here, we report the test results of the flight model of the NISS.

• 천문학회보
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• 제42권1호
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• pp.40.1-40.1
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• 2017

The NISS (Near-infrared Imaging Spectrometer for Star formation history) is the near-infrared spectro-photometric instrument optimized to the Next Generation of small satellite series (NEXTSat). To achieve the major scientific objectives for the study of the cosmic star formation in local and distant universe, the spectro-photometric survey covering more than 100 square degree will be performed. The main observational targets will be nearby galaxies, galaxy clusters, star-forming regions and low background regions. The off-axis optics was developed to cover a wide field of view ($2deg.{\times}2deg.$) as well as the wide wavelength range from 0.95 to $2.5{\mu}m$, which were revised based upon the recent test and evaluation of the NISS instrument. The mechanical structure were tested under the launching condition as well as the space environment. The signal processing from infrared sensor and the communication with the satellite were evaluated after the integration into the satellite. The flight model of the NSS was assembled and integrated into the satellite. To verify operations of the satellite in space, the space environment tests such as the vibration, shock and thermal-vacuum test were performed. The accurate calibration data were obtained in our test facilities. Here, we report the test results of the flight model of the NISS.