• 한국구조물진단유지관리공학회 논문집
• /
• 제25권6호
• /
• pp.50-59
• /
• 2021

현재 공용중인 교량에 대한 재하시험으로 계측한 응답과 초기해석모델의 해석 응답을 비교하여 응답보정계수를 계산하고, 이 모델을 사용하여 내하율과 내하력을 평가하는 방법을 적용하고 있다. 그러나 이러한 응답보정계수는 계측 위치와 하중 조건에 따라 변동하는 값을 준다. 특히 초기해석모델이 교량의 거동에 합당하지 않은 경우, 그 변동 폭이 크며 보정된 모델에 의한 해석 응답이 계측된 응답과 동떨어진 결과를 줄 수 있다. 본 연구에서는 저속으로 주행하는 차량의 다양한 하중 조건에서 동적 성분을 제거한 정적 응답을 얻기 위해 의사정적재하시험법을 적용하였다. 두 개의 유사한 PSC-I 거더교에서 정적 응답을 계측하고, 두 교량 각각에 대한 변위와 변형률에 대한 응답보정계수를 계산하였다. 초기해석모델이 제대로 설정되어 있지 않다면, 평균적으로 구한 응답보정계수로 보정한 모델의 해석 응답이 계측 응답과 오차범위 내에 들어오는지 않음을 확인하였다.

• 대한물리치료과학회지
• /
• 제24권3호
• /
• pp.18-29
• /
• 2017

Purpose: The purpose of this study was to identify the effect of hallux valgus (HV) correction taping on the foot arch and balance of young adults with HV of the big toe. Methods: Forty-eight adults volunteered to participate in this study; of them, the 37 feet (11 men, 26 women) with ${\geq}15^{\circ}$ lateral bending of the metatarsophalangeal joint of the big toe, on a goniometer, were selected as the target foot. Non-elastic correction tape was applied to the foot with HV, while the target foot was used to evaluate the changes, before versus after taping, in the lateral bending angle of the big toe, navicular drop level, Clarke angle, and static balance using a Gaitview system. Each measurement was performed three times, and the average of each set was used in the analysis. The patients'general characteristics were compared by using an independent t-test, and the measurement values were analyzed by using a paired t-test. Results: After taping, the lateral bending angle of the toe significantly decreased (p<.05), difference in navicular drop level significantly decreased (p<.05), the Clarke angle significantly increased (p<.05), and static balance significantly improved (p<.05). Conclusion: We showed that HV taping resulted in an immediately improved HV angle, arch, and single-leg standing balance on the foot with HV. However, further studies should investigate the correlation between HV and foot arch.

• Journal of Power Electronics
• /
• 제14권4호
• /
• pp.742-753
• /
• 2014

In this paper, a new continuously and linearly controlled capacitive static VAR compensator is proposed for the automatic power factor correction of inductive single phase loads in 220V 50Hz power system networks. The compensator is constructed of a harmonic-suppressed TCR equipped with a new adaptive current controller. The harmonic-suppressed TCR is a new configuration that includes a thyristor controlled reactor (TCR) shunted by a passive third harmonic filter. In addition, the parallel configuration is connected to an AC source via a series first harmonic filter. The harmonic-suppressed TCR is designed so that negligible harmonic current components are injected into the AC source. The compensator is equipped with a new adaptive closed loop current controller, which responds linearly to reactive current demands. The no load operating losses of this compensator are negligible when compared to its capacitive reactive current rating. The proposed system is validated on PSpice which is very close in terms of performance to real hardware.

• 한국항공우주학회지
• /
• 제33권4호
• /
• pp.47-56
• /
• 2005

무인기의 INS/GPS/기압고도계 결합항법 시스템에서 수직채널감쇠루프를 사용하여 고도 오차를 보정할 때 비행 고도의 오차를 감소시키기 위해서 기압고도계의 정밀도를 향상시켜야한다. 피토정압관을 사용하여 기압 고도를 측정할 때 비행 속도와 자세 등의 변화에 따라 피토정압관 주위의 압력이 변하여 정압 오차에 의한 기압 고도의 오차를 유발한다. 정압 오차를 보정하기 위하여 풍동 시험과 CFD, 비행 시험 등의 자료를 이용하여 피토정압관 측정 압력의 변화를 분석하고 받음각과 비행 속도에 따른 압력 오차의 모델을 수립하였다. 비행 속도 변화에 의한 오차를 보정하기 위하여 피토정압관의 차압과 차압/정압 비를 사용한 두 가지 오차 모델에 대하여 압력 섭동에 대한 민감도 해석을 하였고 비행 시험에 적용하여 차압/정압 비를 사용한 모델이 고고도 비행 특성이 우수하다는 결론을 얻었다.

• 유체기계공업학회:학술대회논문집
• /
• 유체기계공업학회 2000년도 유체기계 연구개발 발표회 논문집
• /
• pp.226-235
• /
• 2000

Two representative finite volume methods, i.e., the time marching method and the pressure correction method, were applied to 8 centrifugal compressor impeller flows, with low to very high level of pressure ratio, among which 7 impellers' experimental performance is given in the open literature. The present study is focused on the prediction differences from both methods, developed by the authors, in the pressure correction method's point of view. In all cases, the time marching method gives a satifactory solution, but the pressure correction method does not. Up to about $18\%$ less level of total-to-total pressure ratio is predicted by the pressure correction method as the level of the impeller pressure ratio increases up to about 10. The drop of total pressure ratio is caused by the underestimation of static pressure rise which seems to be attributed to inappropriate linearization and discretization of the pressure/density coupling terms in the pressure correction equation.

• Advances in concrete construction
• /
• 제10권1호
• /
• pp.21-34
• /
• 2020

Precast deck joints have larger crack width than cast-in-place concrete decks. The initial crack typically occurs at the maximum moment but cracks on precast joints are significant and lead to failure of the deck. The present crack equation is applied to cast-in-place decks, and requires correction to calculate the crack width of precast deck joints. This research aims to study the crack width correction equation of precast decks by performing static tests using high strength and normal strength concrete. Based on experimental results, the bending strength of the structural connections of the current precast deck is satisfied. However it is not suitable to calculate and control the crack width of precast loop connections using the current design equation. A crack width calculation equation is proposed for crack control of precast deck loop joints. Also included in this paper are recommendations to improve the crack control of loop connections.

• 한국정밀공학회지
• /
• 제14권1호
• /
• pp.205-213
• /
• 1997

In this study, dynamic analysis of a passenger car is carried out to analyze ride quality over a random road profile. The front suspension of the car is a MacPherson strut type and the rear suspension is a multi- link type. The following five different models are constructed and compared to see the effects of engine vibration and chassis flexibility in the ride quality. (1) one rigid chassis model, (2) a rigid chassis and rigid engine model, (3) a rigid engine and flexible chassis model with one vibration mode, (4) one flexible chassis model with six engine vibration modes and one chassis vibration mode, (5) one flexible chassis model with seven vibration modes and four static correction modes. The result shows that engine vibration modes and the first bending mode of the chassis are important in the ride quality.

• Journal of Communications and Networks
• /
• 제7권4호
• /
• pp.489-498
• /
• 2005

For better performance over a noisy channel, mobile wireless networks transmit packets with forward error correction (FEC) code to recover corrupt bits without retransmission. The static determination of the FEC code size, however, degrades their performance since the evaluation of the underlying channel state is hardly accurate and even widely varied. Our measurements over a wireless sensor network, for example, show that the average bit error rate (BER) per second or per minute continuously changes from 0 up to $10^{-3}$. Under this environment, wireless networks waste their bandwidth since they can't deterministically select the appropriate size of FEC code matching to the fluctuating channel BER. This paper proposes an adaptive FEC technique called adaptive FEC code control (AFECCC), which dynamically tunes the amount of FEC code per packet based on the arrival of acknowl­edgement packets without any specific information such as signal to noise ratio (SNR) or BER from receivers. Our simulation experiments indicate that AFECCC performs better than any static FEC algorithm and some conventional dynamic hybrid FEC/ARQ algorithms when wireless channels are modeled with two-state Markov chain, chaotic map, and traces collected from real sensor networks. Finally, AFECCC implemented in sensor motes achieves better performance than any static FEC algorithm.

• 대기
• /
• 제30권4호
• /
• pp.319-333
• /
• 2020

Aircraft observations constitute one of the major sources of temperature observations which provide three-dimensional information. But it is well known that the aircraft temperature data have warm bias against sonde observation data, and therefore, the correction of aircraft temperature bias is important to improve the model performance. In this study, the algorithm of the bias correction modified from operational KMA (Korea Meteorological Administration) global model is adopted in the preprocessing of aircraft observations, and the effect of the bias correction of aircraft temperature is investigated by conducting the two experiments. The assimilation with the bias correction showed better consistency in the analysis-forecast cycle in terms of the differences between observations (radiosonde and GPSRO (Global Positioning System Radio Occultation)) and 6h forecast. This resulted in an improved forecasting skill level of the mid-level temperature and geopotential height in terms of the root-mean-square error. It was noted that the benefits of the correction of aircraft temperature bias was the upper-level temperature in the midlatitudes, and this affected various parameters (winds, geopotential height) via the model dynamics.

• 항공우주시스템공학회지
• /
• 제5권2호
• /
• pp.1-7
• /
• 2011

On this study, applicable aircraft pitot-static system airworthiness requirements and flight test techniques for PEC(Position Error Correction) to KAS Part 23 airworthiness standards are introduced. Also, pros and cons, applicable test conditions, test procedures and required test parameters of each flight test techniques are reviewed on this study.