• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년도 학술대회
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• pp.367-373
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• 2008

Spinning detonations propagating in a circular tube were numerically investigated with a one-step irreversible reaction model governed by Arrhenius kinetics. Activation energy is used as parameter as 10, 20, 27 and 35, and the specific heat ratio and the heat release are fixed as 1.2 and 50. The time evolution of the simulation results was utilized to reveal the propagation mechanism of single-headed spinning detonation. The track angle of soot record on the tube wall was numerically reproduced with various levels of activation energy, and the simulated unique angle was the same as that of the previous reports. The maximum pressure histories of the shock front on the tube wall showed stable pitch at Ea=10, periodical unstable pitch at Ea=20 and 27 and unstable pitch consisting of stable, periodical unstable and weak modes at Ea=35, respectively. In the weak mode, there is no Mach leg on the shock front, where the pressure level is much lower than the other modes. The shock front shapes and the pressure profiles on the tube wall clarified the mechanisms of these stable and unstable modes. In the stable pitch at Ea=10, the maximum pressure history on the tube wall remained nearly constant, and the steady single Mach leg on the shock front rotated at a constant speed. The high and low frequency pressure oscillations appeared in the periodical unstable pitch at Ea=20 and 27 of the maximum pressure history. The high frequency was one cycle of a self-induced oscillation by generation and decay in complex Mach interaction due to the variation in intensity of the transverse wave behind the shock front. Eventually, sequential high frequency oscillations formed the low frequency behavior because the frequency behavior was not always the same for each cycle. In unstable pitch at Ea=35, there are stable, periodical unstable and weak modes in one cycle of the low frequency oscillation in the maximum pressure history, and the pressure amplitude of low frequency was much larger than the others. The pressure peak appeared after weak mode, and the stable, periodical unstable and weak modes were sequentially observed with pressure decay. A series of simulations of spinning detonations clarified that the unsteady mechanism behind the shock front depending on the activation energy.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년 추계학술대회논문집
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• pp.367-373
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• 2008

Spinning detonations propagating in a circular tube were numerically investigated with a one-step irreversible reaction model governed by Arrhenius kinetics. Activation energy is used as parameter as 10, 20, 27 and 35, and the specific heat ratio and the heat release are fixed as 1.2 and 50. The time evolution of the simulation results was utilized to reveal the propagation mechanism of single-headed spinning detonation. The track angle of soot record on the tube wall was numerically reproduced with various levels of activation energy, and the simulated unique angle was the same as that of the previous reports. The maximum pressure histories of the shock front on the tube wall showed stable pitch at Ea=10, periodical unstable pitch at Ea=20 and 27 and unstable pitch consisting of stable, periodical unstable and weak modes at Ea=35, respectively. In the weak mode, there is no Mach leg on the shock front, where the pressure level is much lower than the other modes. The shock front shapes and the pressure profiles on the tube wall clarified the mechanisms of these stable and unstable modes. In the stable pitch at Ea=10, the maximum pressure history on the tube wall remained nearly constant, and the steady single Mach leg on the shock front rotated at a constant speed. The high and low frequency pressure oscillations appeared in the periodical unstable pitch at Ea=20 and 27 of the maximum pressure history. The high frequency was one cycle of a self-induced oscillation by generation and decay in complex Mach interaction due to the variation in intensity of the transverse wave behind the shock front. Eventually, sequential high frequency oscillations formed the low frequency behavior because the frequency behavior was not always the same for each cycle. In unstable pitch at Ea=35, there are stable, periodical unstable and weak modes in one cycle of the low frequency oscillation in the maximum pressure history, and the pressure amplitude of low frequency was much larger than the others. The pressure peak appeared after weak mode, and the stable, periodical unstable and weak modes were sequentially observed with pressure decay. A series of simulations of spinning detonations clarified that the unsteady mechanism behind the shock front depending on the activation energy.

• 한국방사선학회논문지
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• 제13권5호
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• pp.705-711
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• 2019

현재 최신 장비의 두부 CT검사에서 파라메타의 변화와 선량변화에 대한 연구가 부족하고 특히 노이즈, 균일도 해석 및 선량변화에 대한 연구가 부족하다고 생각된다. 따라서 높은 사양 두부 CT 사용 시 노출 파라메타 중 관전압, 슬라이스 두께, 피치변화에 대해 분석하여 이때 발생하는 현상에 대해서 연구하고자 하였다. 실험을 통해서 균일도는 고관전압과 두꺼운 슬라이스 선택 및 최저 피치를 사용할 때 균일도가 좋음을 알 수 있었다. 모두 조합한 결과 균일도가 가장 조건은 140 kVp, 10 mm, pitch 0.5로 나타났다. 노이즈는 관전압과 슬라이스 두께를 높이면 피치에 관계없이 개선되는 것을 알 수 있었고, 선량은 관전압과 피치의 증가에 따라 선형적으로 증가하는 것으로 나타났다. 따라서 본 연구결과는 고 사양의 두부 CT 사용에서 참고자료가 될 것이다.

• 한국방사선학회논문지
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• 제15권4호
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• pp.437-444
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• 2021

두경부 CT 검사시 팬텀을 이용하여 Helical mode, High Pitch Mode, Volume Axial Mode 사용하여 획득한 CT 영상으로부터 환자의 피폭선량과 각 영상의 화질을 비교 및 분석하여 Volume Axial Mode의 유용성을 평가해보고자 한다. 두경부 CT 검사 시 각 mode에 따른 70 kVp, 80 kVp, 100 kVp 관전압에 따라 검사를 시행하였다. 사용 장비로는 GE사의 Revolution(GE Healthcare, Wisconsin USA) 모델과 iMED X-ray Phantom을 이용하였다. 검사 Mode에따른 kVp별로 얻어진 영상을 이용하여 팬텀의 피폭선량을 비교하였으며, 각 영상에 ROI를 설정해 신호대 잡음비와 대조도대 잡음비를 산출하여 영상의 화질을 비교하였다. Volume Axial Mode를 사용하여 검사하였을 때 팬텀의 피폭선량이 Helical에 비해 17.12% 낮게, High Pitch에 비해 5.35% 낮게 측정되었고, 신호대 잡음비와 대조도대 잡음비가 향상되었다. Volume Axial Mode는 고속 회전 스캐너를 이용하여 테이블의 이동이 없이 조사시간을 줄이고, High Pitch Mode와 Helical Mode를 사용했을 때 보다 팬텀의 0.28초의 단시간에 영상을 획득하여 피폭선량이 감소하고 영상의 화질 또한 향상되는 유용한 검사라 할 수 있다. 또, 몸이 불편한 환자의 촬영이나 긴급환자의 CT 촬영에 있어서 Volume Axial Mode의 빠른 검사시간은 최대의 장점이라고 볼 수 있다.

• 음성과학
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• 제15권3호
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• pp.175-181
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• 2008

The aim of this study was to survey 'voice preference' of children from among three voice pitches, which are high-pitch, mid-pitch and low pitch, and understand acoustic characteristics of the best voice chosen. To record distinctive pitches, Dr. Speech(ver. 4.0 Tiger Electronics) was used and we analyzed their choices. Also, we measured subglottal air pressure in aerodynamic analyze and phonatory aerodynamic system(Model 6600, KAY) was used. As a result children preferred to the low-pitch yet there was not any difference by sex. We fined them to prefer higher HNR voice to lower jitter and shimmer voice rate.

• 한국생산제조학회지
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• 제24권3호
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• pp.355-362
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• 2015

Test procedure for the design verification of wind turbine pitch and yaw bearings has been developed. Test items were selected to evaluate operational reliability of pitch and yaw bearings by considering loading and operational conditions, and by analyzing the design criteria of pitch and yaw bearings. The developed test items consisted of preliminary test, fatigue load test, extreme load test, low temperature environmental test and dismantling inspection after all the test were completed. Because it reflects the actual operational conditions of the pitch and yaw bearings, the developed test procedure has high reliability and can verify the basic design considerations in the international standard and guidelines.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2002년도 합동 추계학술대회 논문집 정보 및 제어부문
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• pp.529-532
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• 2002

This research treated development of real time pitch tracer for training of musical tune of speech signal and pre-processing and post-processing technics were proposed to get higher accuracy in extraction of pitch. Autocorrelation Function was used to get pitch frequency from 64Hz to 980Hz in real time. Half Rectifier method and Envelop extraction method as a pre-processing was used to get higher accuracy in pitch detection, and improved results were obtained on noised speech signal. Post-processing method using periodicity of Autocorrelation was proposed to get higher accuracy in the high frequency region.

• 대한기계학회논문집A
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• 제38권6호
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• pp.609-617
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• 2014

풍력터빈 블레이드의 가변 피치제어는 풍력발전기의 과풍속 영역 설계에 있어 중요한 요소로 알려져 있으나 원가문제 때문에 소형 풍력터빈에는 적용되지 못하고 실속제어가 많이 적용되고 있다. 하지만, 블레이드 주변의 난류 때문에 설계된 실속이 구현되지 않는 실속지연 현상이 종종 발생되고, 이에 따른 풍력 블레이드의 과회전과 발전기의 과출력 위험이 발생하고 있다. 이에 따라 블레이드에서 발생되는 공력으로 피치가 변하고 스프링의 복원력으로 복귀되는 수동형 피치제어 모듈이 주목 받고 있다. 본 연구에서는 회전하는 블레이드의 익형에서 발생되는 양력과 항력을 이용하여 회전면으로 작용되는 토크와 블레이드의 Flap 방향으로 작용되는 추력을 계산하는 방법을 제시하고, 이러한 힘들의 크기를 여러 가지 익형에 대해 비교하였으며, 블레이드의 피치모멘트를 정량적으로 산출하여 수동 피치제어 모듈의 설계자료로 활용될 수 있도록 하였다.

• Carbon letters
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• 제2권3_4호
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• pp.182-191
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• 2001

Quinoline insoluble formed by the heat treatment was hot-pressed near its softening point. The green body was stabilized in the temperature range of $300{\sim}400^{\circ}C$ and subsequently carbonized below $1300^{\circ}C$ in an argon atmosphere. The behaviors of QI formation was examined with varying the heat treatment temperature and the lapse of time of the sample carbonized at various temperatures. And the mechanical property, corrosion resistance, and friction behavior were also measured optimum content of mesophase pitch ensured a dense structure and high $LC_{(002)}$ value, which resulted in high mechanical properties, good corrosion resistance, and low-stable friction behavior.

• 전기학회논문지
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• 제66권10호
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• pp.1523-1531
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• 2017

In general, the thrust vector control should be fast and stable in the initial launch phase. Two types of conventional controllers, one is for pitch angle control and the other is for pitch rate control, are designed based on the equation of motion without aerodynamics and are compared in the viewpoints of the stability margin and the time response performance. Also analyzed are the rejection capabilities to cope with high aerodynamic disturbances caused by high angle of attacks in initial booting phase. Additionally, time response features at actuator saturation are investigated. Based on those results, we suggest a controller structure which is more suitable for thrust vector control of missiles at initial booting phase.