• 한국자기학회지
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• 제21권6호
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• pp.219-224
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• 2011

해부학적 기술로 경락의 실체인 프리모 시스템 내에 존재하는 산알을 획득하여 운동 모습을 광학 현미경으로 분석하였고, 낮은 정자기장하에서 운동 특성을 조사하였다. 토끼 장기 표면으로부터 산알이 다량으로 몰려있는 프리모 소체 내에 약 1 ${\mu}m$ 정도 크기의 산알들을 선택 및 분리시켜, 패트리 디쉬 안에 PBS 용액과 산알을 담았다. 내부 온도 $38^{\circ}C$, 100 Oe 이하 일정한 외부 자기장에 평행방향과 수직방향으로 움직이는 산알의 운동속도를 관찰하였다. 평행방향 외부 자기장이 0 Oe에서 80 Oe까지 20 Oe 증가함에 따라 5개 산알 중 4개는 약 0.9 pixel/s의 평균속도로 감소하는 뚜렷한 경향성을 갖고 있음을 볼 수 있었다. 반면에 수직 방향으로 운동하는 산알의 경우, 외부 자기장이 없을 때와 비슷한 무작위로 운동함을 관찰하였다. 이러한 실험결과로부터 산알 핵 DNA내에 망간(Mn)과 코발트(Co) 등의 다량의 무기물을 함유하는 산알이 회전운동을 하면서 움직일 때, 외부 자기장을 인가함으로써 운동 특성을 약화시키는 자기적 특성이 있는 것으로 사료되었다.

• 천문학회지
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• 제38권2호
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• pp.237-240
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• 2005

We present images of L1551 IRS5 at angular resolutions as high as ${\~}$30 mas, corresponding to a spatial resolution of ${\~}$5 AU, made at 7 mm with the VLA. Previously known to be a binary protostellar system, we show that L1551 IRS5 is likely a triple protostellar system. The primary and secondary components have a projected separation of ${\~}$46 AU, whereas the tertiary component has a projected separation of ${\~}$11 AU from the primary component. The circumstellar dust disks of the primary and secondary components have dimensions of ${\~}$15 AU, whereas that of the tertiary component has a dimension of ${\~}$10 AU. Their major axes are closely, but not perfectly, aligned with each other, as well as the major axis of the surrounding flattened, rotating, and contracting molecular condensation (pseudodisk). Furthermore, the orbital motion of the primary and secondary components is in the same direction as the rotational motion of this pseudodisk. We suggest that all three protostellar components formed as a result of the fragmentation of the central region of the molecular pseudo disk. The primary and secondary components, but apparently not the tertiary component, each exhibits a bipolar ionized jet that is centered on and which emergers perpendicular to its associated dust disk. Neither jets are resolved along their base, implying that they are driven within a radial distance of ${\~}$2.5 AU from their central protostars. Finally, we show evidence for what may be dusty matter streams feeding the two main protostellar components.

• 대한기계학회논문집A
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• 제26권8호
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• pp.1527-1533
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• 2002

When a mechanism transfers a motion to an intersected shaft, a cylindrical cam mechanism may be the best choice among the mechanisms. The cylindrical cam with a roller follower provides to transfer the motions to the intersect shafts simply without other connecting equipments of the intersect shafts. Typical example may be a roller-gear-cam mechanism. But the shape of the cam must be exactly defined in order to satisfy the conditions for the prescribed motion of the follower. This paper proposes a new method for the shape design of the cylindrical cams and also a CAD program is developed by using the proposed method. The relative velocity method calculates the relative velocity of the follower versus the cam at a center of roller, and then determines a contact point by using the geometric relationships and the kinematic constraints. The constraint used in the relative velocity method is that the relative velocity must be parallel to a common tangent line at the contact point of two independent bodies, i. e. the cam and the follower. Then, the shape of the cam is defined by the coordinate transformation of the trace of the contact points. Finally, this paper presents an example in order to prove the accuracy of the proposed methods in this paper and the application of the CAD program"CamDesign".

• 대한물리의학회지
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• 제15권1호
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• pp.19-24
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• 2020

PURPOSE: This paper describes the effects of the myofascial release (MFR) approach in a 20-year-old female patient with neuroforaminal encroachment and regional kyphosis in the cervical area, who also had neck pain. METHODS: A 20-year-old female presented with the chief complaint of neck pain while studying with a level of seven on the rating analogue scale (RAS) and was not taking any drugs or undergoing treatment for the control of neck pain prior to visiting. The cervical radiograph demonstrated neuroforaminal encroachment from C4-5. The patient showed 3.5° kyphosis at C4-5 and 22.9° lordosis at C2-7 according to the Harrison posterior tangent method. The anterior head translation (AHT) was 13.9mm. She reported pain of RAS 5 at the scapular medial border while rotating her neck in the left direction and flexing forward. The patient was treated a total 16 times, three times/week for six weeks using the MFR approach. RESULTS: After the treatment sessions, studying without pain was possible for approximately two hours, but after approximately two hours of studying, she experienced pain of RAS 6 and a stiff feeling in front of the neck. Neuroforaminal encroachment was not detected in the radiographs taken after applying MFR. Improvement of C4-5 kyphosis was noted (from 3.5° kyphosis to 3.8° lordosis). AHT was decreased by 13.6 mm (from 13.9 mm to 0.3 mm). The pain with motion had disappeared. CONCLUSION: The MFR approach in this patient with neuroforaminal encroachment could reduce the pain related to motion and restore the regional cervical lordosis.

• 한국항공우주학회지
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• 제31권6호
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• pp.1-7
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• 2003

본 연구에서는 3차원 대칭형 날개의 정상/비정상상대에서의 공기력 특성을 Vortex 패널법을 이용하여 수치적으로 연구했다. 이 프로그램은 날개 표면에 분포된 x, y 방향에 따라 선형적으로 변화는 와(Vortex)를 이용하는 프로그램을 기반으로 하여 3차원 날개 주위의 비압축성 포텐셜 흐름에 적용하였고 박리와 후류의 변형은 고려하지 않았다. NACA Airfoil 자료와 비교한 계산결과는 매우 만족스러운 일치를 보여주었다. 또한 갑작스러운 pitch-up운동과 일정한 각속도로 피칭운동을 하는 비정상 날개에 대해서도 본 방법을 적용하였다. 비정상 상태의 연구에서는 출발와류의 생성과 시간에 따른 위치를 고려함으로서 출발와류가 날개의 공기력 특성에 미치는 영향을 계산하였다. 본 방법은 피칭이나 플래핑, 회전익 해석등의 더 복잡한 경우에도 적용되어질 수 있다.

• International Journal of Fluid Machinery and Systems
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• 제1권1호
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• pp.1-9
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• 2008

In the first part of the paper, Computational Fluid Dynamics analysis of the combusting flow within a high-swirl lean premixed gas turbine combustor and over the $1^{st}$ row nozzle guide vanes is presented. In this analysis, the focus of the investigation is the fluid dynamics at the combustor/turbine interface and its impact on the turbine. The predictions show the existence of a highly-rotating vortex core in the combustor, which is in strong interaction with the turbine nozzle guide vanes. This has been observed to be in agreement with the temperature indicated by thermal paint observations. The results suggest that swirling flow vortex core transition phenomena play a very important role in gas turbine combustors with modern lean-premixed dry low emissions technology. As the predictability of vortex core transition phenomena has not yet been investigated sufficiently, a fundamental validation study has been initiated, with the aim of validating the predictive capability of currently-available modelling procedures for turbulent swirling flows near the sub/supercritical vortex core transition. In the second part of the paper, results are presented which analyse such transitional turbulent swirling flows in two different laboratory water test rigs. It has been observed that turbulent swirling flows of interest are dominated by low-frequency transient motion of coherent structures, which cannot be adequately simulated within the framework of steady-state RANS turbulence modelling approaches. It has been found that useful results can be obtained only by modelling strategies which resolve the three-dimensional, transient motion of coherent structures, and do not assume a scalar turbulent viscosity at all scales. These models include RSM based URANS procedures as well as LES and DES approaches.

• 대한조선학회논문집
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• 제50권3호
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• pp.138-144
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• 2013

New experimental devices and methods to measure shaft forces of ships are proposed in this paper. The strain gauge type six-component load cell was newly designed and installed to the end of the propeller shaft. The signals generated from the sensor in the propeller rotating are transferred to the new data amplifying and processing board on the shaft and the data is transmitted to the self-made wireless receiver. To find out the characteristics of shaft forces during port and starboard turning motions in sea trial, oblique and combined yaw maneuvering tests at straight, transient, maximum yaw rate, steady conditions were performed with the model ship installed the shaft forces measuring device using circular motion tester of Samsung Ship Model Basin. Characteristics of the measured shaft forces in model tests show quantitatively good agreement with the computed values obtained by the CFD programs using the measured wake data in oblique towing conditions. In the near future, It is hoped that the estimated shaft forces for a ship from this experimental method could be validated through comparison with directly measured values of a ship.

• 대한방사선기술학회지:방사선기술과학
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• 제21권1호
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• pp.29-34
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• 1998

The purpose of simple abdomen erect projection is to see the fluid level which indicates gastrointestinal ileus or free air due to perforation. we do not have to insist on low kVp technique in simple abdomen erect position as long as we can detect the fluid level and free air shadow. Therefore, the author tried to decrease patient dose by high kVp technique and to improve the image quality due to motion artifact by reduction of exposure time. [Methods] Experiment 1. * screen/film SRO1000/HRH * exposure factor : $140\;kvp{\pm}5\;kv$ with added filters, 200 mA, 0.01 sec * phantom : Acryles : 15.0 cm(equivalent to 17 cm body thickness) 17.5 cm(equivalent to 21 cm body thickness) 20.0 cm (equivalent to 25 cm body thickness) With the exposure factor for same film density($D=0.8{\pm}0.1$) and with the materials above, we tried to find out entrance skin dose and gonad dose for both male and female. Experiment 2. Burger's phantom radiography were checked to see whether there was any change of image quality according to the kVp and the added filters. Experiment 3. Using rotating meter(self made), we examined the motion artifact and the exposure time limitation. [Results and conculution] 1. Using high voltage technique of 140 kVp with added filter, Skin dose, testicle dose and ovary dose decrease to 89.3%, 47% and 71.4% respectively compare to 70 kVp technique, 2. No great changes of Burger's phantom image has detected as from 70 kVp to 140 kVp and the air hole size of Burger's phantom over 0.028 cc(Diameter 3 mm, hight 4 mm) can be distinghished. 3. 0.01 sec(1 pulse) exposure time is possible in the single phase full wave rectification that why we can quitely reduce the unsharness caused by patient's movement.

• 한국운동역학회지
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• 제20권4호
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• pp.429-436
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• 2010

The purpose of this study was to analyze the kinematic factors and throwing variables for the 3-turn and 4-turn techniques and for release as well as to provide technical advice for improving athletic performance in hammer throwing. Data analysis led to the following conclusions: To increase the rotation speed for the 3-turn and 4-turn techniques, the time elapsed during the 1-foot support period should be decreased the distance between the rotating foot and the rotation axis should be small and the height of the hip joint should be increased at the times of release The throwing angle at the moment of release should be more than 40 degrees, and the throwing position should be taken vertically high at the shoulder joints. To accelerate the motion of the hammer, the speed should not be reduced during the 1-foot support period but should be increased during the 2-foot support period for much greater acceleration. In the 3-turn technique, the angles of the shoulder axis and hummer string should be dragged angle at the maximum point and lead angle at the minimum point, and dragged angle at the maximum and minimum points in the 4-turn at the time of relase The upper body should be quickly bent backward, the knee angle should be extended, and the angles of the shoulder axis and hammer string should be dragged angle close to 90 degrees.

• 대한조선학회논문집
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• 제55권6호
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• pp.474-481
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• 2018

This paper is to compare by numerical analysis the flow characteristics and propulsion performance of stern with the shape change of K-duct, a pre-swirl duct developed by Korea Research Institute of Ships & Ocean Engineering (KRISO). First, the characteristics of the propeller and the resistance and self-propulsion before and after the attachment of the K-duct to the ship were verified and the validity of the calculation method was confirmed by comparing this result with the model test results. After that, resistance and self-propulsion calculations were performed by the same numerical method when the K-duct was changed into five different shapes. The efficiency of the other five cases was compared using the delivery horsepower in the model scale and the flow characteristics of the stern were analyzed as the velocity and pressure distributions in the area between the duct end and the propeller plane. For the computation, STAR-CCM +, a general-purpose flow analysis program, was used and the Reynolds Averaged Navier-Stokes (RANS) equations were applied. Rigid Body Motion (RBM) method was used for the propeller rotating motion and SST $k-{\omega}$ turbulence model was applied for the turbulence model. As a result, the tangential velocity of the propeller inflow changed according to the position angle change of the stator, and the pressure of the propeller hub and the cap changes. This regulated the propeller hub vortex. It was confirmed that the vortex of the portion where the fixed blade and the duct meet was reduced by blunt change.