• 천문학회지
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• 제29권spc1호
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• pp.439-440
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• 1996

The Chinese ancient accounts of timing observations of 48 lunar eclipses and the secular variation of the Earth's spin speed are discussed. A series of ${\Delta}$T expressing the secular deceleration of the Earth's rotation was obtained. The average increase rate of length of the day is about 1.5 milliseconds per century.

• 한국세라믹학회지
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• 제53권1호
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• pp.81-86
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• 2016

The effect of substrate rotation speed on the phase forming behavior and microstructural variation of 8 wt% yttria ($Y_2O_3$) stabilized $ZrO_2$ (8YSZ) coatings as a thermal barrier coating has been investigated. 8YSZ coatings with $100{\sim}200{\mu}m$ thickness were deposited by electron beam-physical vapor deposition onto a super alloy (Ni-Cr-Co-Al) substrate with a bond coating (NiCo-CrAlY). The width of the columnar grains of the 8YSZ coatings increased with increasing substrate rotation speed from 1 to 30 rpm at a substrate temperature range of $900{\sim}950^{\circ}C$. In spite of the different growth behaviors of coatings with different substrate rotation speeds, the phases of each coating were not changed remarkably. Even after post heat treatments with various conditions of the coated specimens fabricated at 20 rpm, only a change of color was noticeable, without any remarkable change in the phase or microstructure.

• 대한전자공학회논문지SD
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• 제41권12호
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• pp.75-81
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• 2004

AE-CORDIC은 CORDIC 연산의 회전 방향을 미리 계산하는 알고리즘을 이용해 CORDIC의 연산속도를 향상 시켜준다. 회전방향을 예측할 수 없는 부분은 Lookup-Table로 대체하고, 예측 가능 부분만을 CORDIC 으로 처리하였는데, 회전방향 예측은 별도의 추가 하드웨어 없이 간단하게 인코딩 할 수 있게 된다. 그리고, Unrolled CORDIC 구조에서는 Lookup-Table입력 비트 수가 크지 않으면 Lookup-Table의 하드웨어 증가보다 CORDIC 연산 단에서 감소되는 ADDER의 하드웨어가 더 크기 때문에 오히려 전체 하드웨어 크기가 줄어든다. 본 논문에서는 회전방향 예측 가능 구간 및 예측 방법을 제안하고, 최적화된 Lookup-Table의 크기를 결정하여 기존의 회전방향 예측 알고리즘인 P-CORDIC 과 비교하였다. 그리고, 입력 각이 16비트 경우를 삼성 0.18㎛ 공정을 이용해 논리 합성하여 하드웨어 크기, 성능, 정확성을 검증하였다.

• 한국항공운항학회지
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• 제17권4호
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• pp.70-75
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• 2009

According to the aviation statistics, tail strike incidents and accidents are cyclic. Although many tail strikes occurred during takeoff, these are less than during landing cases. Many cases are related on human factors. In my opinion it is possible to analyze the causes of takeoff tail strikes to some extent. There are major casual factors of tail strike during takeoff such as; (1) Mis-trimmed horizontal stabilizer (2) premature rotation prior to $V_R$ (3) Excessive pitch up rate during rotation (4) Improper use of the flight director. Among these causes improper use of flight director is excluded in this paper because it is recommended that pilot should use flight director after airborne. So I analyzed the other three causes as following. Firstly, because mis-trimmed stabilizer is related to center of gravity(CG), the relationship between stabilizer and CG is reviewed. Secondly, concerned premature rotation prior to $V_R$ I reviewed the background of rotation speed($V_R$) establishment and analyzed theoretically what speed leads to tail strikes. Thirdly, concerning excessive pitch up rate during rotation I analyzed what excessive pitch up rate can decrease ground clearance while using FDR data.

• 한국운동역학회지
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• 제16권1호
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• pp.55-63
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• 2006

The purpose of this study is to prove the kinematical characteristics of Deff motion, the high bar performance, in terms of flying phases so that we can provide basic sources for improving gymnastic performance. To do this, we selected and analyzed the performance of two athletes who did Deff motion in the high bar competition of male artistic gymnastic in the 22nd Universiade 2003 Daegu. We drew the conclusions from the kinematical factors that were came out through analyzing three-dimensional cinematography of the athletes' movements, by using a high speed video camera. To make a successful performance, a performer releases the bar at a height of a high bar vertically and at a height of 82cm horizontally, and the flying performance should be made without moving forward, as maintaining the proper balance, in order to rise over 118cm high during the flying phase. When the performer is releasing the bar, an increase of the vertical speed in the center of the body and extension of a knee joint and a hip joint contribute to increasing a flying height. And when the moving body is twisted, leaning to left side is caused by the winding movement of a knee joint, which causes an unstable bar grasp. To grasp the bar stably, just before releasing the performer should gain propulsive force from twisting rotation through increasing the speed of shoulder rotation. And before the peak point, the performer should make sure of a body rotation distance over $164^{\circ}$ so that he or she can do an aerial rotary performance smoothly. When grasping the high bar, the center of the body should be above the bar and the angle of shoulder rotation should be maintained close to $540^{\circ}$ simultaneously. he high point performance(S1) has more speed on an ascending phase and less speed on a descending phase than the low point performance (S2). At the peak point, both the rotation angle of the body and that of the shoulder in high point performance are big as well. In conclusion, it is shown that a performer can make a jump toward the high bar easily with the body straight because the performer can hold the upper part of the body erect early in a descending phase.

• 한국주조공학회지
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• 제43권6호
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• pp.271-278
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• 2023

본 연구에서는 임펠러 회전속도와 불활성 가스 유량을 바꾸어가며 A356 용탕 탈가스 실험을 수행하여 탈가스 시간에 따른 용탕 온도, 성분 및 밀도 변화를 측정하였다. 용탕 온도의 경우 탈가스 처리가 진행됨에 따라 서서히 감소하였으나 임펠러 회전속도 혹은 불활성 가스 유량과 용탕 열손실 간의 뚜렷한 상관관계는 확인할 수 없었다. 임펠러 회전속도와 불활성 가수 유량에 상관없이, A356 용탕 내 Mg 및 Ti 함량은 600초 이상 탈가스 처리 후에도 그 함량이 거의 변하지 않았으며, Sr의 경우 최대 70 ppm정도 그 함량이 낮아지는 것을 확인하였다. 측정된 용탕 밀도로부터 도출한 용탕 내 수소 농도와 탈가스 모델 식을 활용하여 실험 조건 별 탈가스 속도를 정량적으로 비교 분석해본 결과, 본 연구에서 다룬 탈가스 조업 환경에서는 임펠러 회전속도 보다는 불활성 가스 유량이 탈가스 속도에 영향을 미치는 것을 확인할 수 있었다.

• 한국철도학회:학술대회논문집
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• 한국철도학회 2011년도 정기총회 및 추계학술대회 논문집
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• pp.1583-1593
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• 2011

As we see the continuation of the increase in the speed of the High Speed railroad worldwide, there is a concern for a possible problem in the connecting transition zone in the railway infrastructure. Honam High Speed railroad's transition zone in the hub for the rotation structures and other supporting structures such as approach slab, sub slab, approach block, etc. Due to its increase in speed of the design speed, and its important role on the driving stability and credibility of the bearing ground performance, we must seek and fine a prevention plan for a cause of differential settlement, as well as the cause of the derailment. In this dissertation, domestic, as well as international design manuals and the applicability of the control standards are studied. Also through the study target, Honam High Speed railroad zone 4-1, we evaluated the connecting componant of the Yeon-Jeong bridge through the eigenvalue and weight transfer of the train when operated at 300km/h, 350km/h, 400km/h, 450km/h, and were able to achieve detailed assessment by checking track behaviors, looking at various components such as the rotation acceleration according to the inversion of the distance length, displace length, displacement and stress distribution. Through these studied, possibility of operating at 400km/h was evaluated based on the condition of the current design basis.

• 한국생산제조학회지
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• 제7권1호
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• pp.51-57
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• 1998

In order to minimize vibration problems of rotating machinery rotors have been assembled through balancing machines. Since perfect balancing is impossible, residual unbalances cause serious vibration while the rotor is in high speed region. To minimize unbalance effects of magnetic bearing systems (AMB) during rotation on-line balancing methodology was studied. Unbalances were considered as disturbances of the system. The disturbance observer was used to estimate unbalance force from measurable state and input variables. Balancing inputs computed according to LQR and outputs of the observer were applied to eliminate unbalances during high speed rotation of the AMB. the effectiveness of the on-line balancing was verified through numerical simulations.

• 대한설비공학회:학술대회논문집
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• 대한설비공학회 2009년도 하계학술발표대회 논문집
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• pp.1391-1396
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• 2009

The direct drive motor used in a precision motion rotate at about 1/10 speed and high torque comparing with general rotary motor. Excessive heating of the coils cause an exacerbating the heat problems and reducing the performance of motor. Because the rotation speed of the rotor and surrounding air is low, the motor can not be inefficiently cooled, the thermal analysis in the motor is very important. As the variations of rotation speed and torque, the temperature of several parts is measured and the features of the heat transfer is analyzed and improved.

• 대한용접접합학회:학술대회논문집
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• 대한용접접합학회 2005년도 추계학술발표대회 개요집
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• pp.132-134
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• 2005

The friction surfacing system which has been successfully developed in RIST has both position control and force control by using hydraulic cylinder. In friction surfacing process mechtrode rotation speed(N) and feeding speed($V_{z}$), travelling speed($V_{x,y}$) are of critical importance for the width and thickness of the coating. As a result of DOE with developed system, the main effect of coating thickness is a rotation speed of mechtrode.