• 제목/요약/키워드: Angle velocity

검색결과 2,080건 처리시간 0.028초

Ultrasonic Measurement of Tissue Motion for the Diagnosis of Disease

  • Beach Kirk W.
    • International Journal of Vascular Biomedical Engineering
    • /
    • 제1권1호
    • /
    • pp.3-12
    • /
    • 2003
  • Ultrasonic pulsed Doppler velocimetry has become a standard international method of classifying carotid disease. Because the measured angle adjusted velocity increases as the Doppler angle increases, examinations should be performed at a convenient standard Doppler examination angle. An angle of 60 degrees is achievable throughout most examinations. Multiple Doppler viewing angles allow the acquisition of velocity vectors during the cardiac cycle, revealing the complex velocity patterns. Ultrasonic velocimetry (whether Doppler or time domain) is based on changes in the phase of the ultrasound echo. Other examinations can be done based on the echo phase. Slow motions of organs such as the brain can be used to monitor changes in edema. Measurements of tissue strain due to the pulsatile filling of the arterioles. This plethysmographic imaging method can display differences in tissue perfusion because of different tissue types and changes in autonomic activity.

  • PDF

삼지화염의 전파속도에 대한 속도구배의 영향에 관한 실험적 연구 (Experimental Study on the Effect of Velocity gradient on Propagation speed of Ttribrachial flame in Laminar Coflow Jets)

  • 김민국;원상희;정석호
    • 한국연소학회:학술대회논문집
    • /
    • 한국연소학회 2005년도 제31회 KOSCO SYMPOSIUM 논문집
    • /
    • pp.221-228
    • /
    • 2005
  • The tribrachial flame in laminar coflow jet has been investigated experimentally with unsteady propagating condition. In this experiment, we found that the tribrachial point has an angle of flame surface because the location of tribrachial point is not on the base point of flame but on the inclined surface of flame. This angle of Flame surface at tribrachial point are increasing when the flame is approaching to the nozzle exit. With considering this angle of flame surface, the radial velocity gradient can affect flame propagation speed by increasing flow-stretch effect. The propagation speed of tribrachial flame was calculated with including above stretch effect. The speed decreases with increasing velocity gradient due to the increment of stretch effect.

  • PDF

피치제어형 풍력발전시스템의 속도제어 (Speed Control of a Wind Turbine System Based on Pitch Control)

  • 임종환;허종철
    • 제어로봇시스템학회논문지
    • /
    • 제7권2호
    • /
    • pp.109-116
    • /
    • 2001
  • The paper presents a speed control algorithm for a full pitch-controlled wind turbine system. Torque of a blade generated by wind energy is a nonlinear function of wind speed, angular velocity, and pitch angle of the blade. The design of the controller, in general, is performed by linearizing the torque in the vicinity of the operating point assuming the angular velocity of the blade is constant. For speed control, however the angular velocity is on longer a constant, so that linearization of the torque in terms of wind speed and pitch angle is impossible. In this study, a reference pitch model is derived in terms of a wind speed, angular velocity, and pitch angle, which makes it possible to design a controller without linearizing the nonlinear torque model of the blade. This paper also suggests a method of designing a hydraulic control system for changing the pitch angle of the blade.

  • PDF

충돌분류에 의한 액적의 크기 및 속도특성에 관한 실험적 연구 (An Experimental study on the drop size and velocity characteristic of drop by impinging jets)

  • 한재섭;김선진
    • 한국분무공학회지
    • /
    • 제4권4호
    • /
    • pp.30-37
    • /
    • 1999
  • The breakup characteristics of liquid sheet formed by the liquid rocket injector has a close relation with the combustion efficiency. In this paper, basic characteristics of droplet size and velocity distribution were measured with PDPA for the Like Doublet Impinging Injector. Test variables were the angle of impact, the diameter of orifice and jet velocity. Water was used as test fluid. As a result, for impingement angle less than 90 degree, following correlations were obtained between drop size and design parameters : $D_{32}({\mu}m)=295.0{\times}V^{-0.09}\times(2\theta)^{-0.1}{\times}d^{0.072}$. For impingement angle greater than 100 degree, drop sizes were increased but eventually converged to a certain limiting value.

  • PDF

수치해석을 이용한 인공절리 조건에 따른 발파속도 평가 (Evaluation of Blast Velocity by Artificial Joint Conditions using Numerical Analysis)

  • 석철기;노유송;박훈
    • 화약ㆍ발파
    • /
    • 제35권4호
    • /
    • pp.1-9
    • /
    • 2017
  • 본 연구는 인공절리를 이용한 발파효과 검토를 위해 인공절리 수, 인공절리 간격, 인공절리 경사에 따른 발파속도의 영향 및 기여도를 평가 분석한 연구이다. 인공절리 상태 변화에 따른 발파속도는 동적해석 프로그램인 AUTODYN을 이용하여 획득하였다. 수치해석 결과에 대해 정규화 분석을 수행하였고, 각 인자의 기여도 분석을 위해 강건설계 실험계획법을 이용하여 설계 인자를 분석하였다. 각 인자는 3수준으로 설정하였고, 분석에 직교 배열표 $L_9(3^4)$를 사용하였다. 정규화 분석을 통해 수치해석 결과를 분석한 결과 인공절리 경사가 증가함에 따라 발파속도는 감소하는 경향을 보였다. 또한, 인공절리 간격과 인공절리 경사에 대해 발파속도를 분석한 결과 발파속도는 경사가 수직일 때 인공절리 간격이 증가함에 따라 감소는 경향을 보였다. 강건설계를 이용한 기여율 분석결과 발파속도에 가장 큰 영향을 미치는 것은 인공절리 경사이며, 이어서 인공절리 수, 인공절리 간격 순으로 기여율이 평가되었다.

정상유동 장치에서 유동 특성 평가 방법에 대한 연구(4) - 유속분포(2) (Study on Evaluation Method of Flow Characteristics in Steady Flow Bench(4) - Velocity Profile(2))

  • 박찬준;성재용;엄인용
    • 한국자동차공학회논문집
    • /
    • 제24권2호
    • /
    • pp.242-254
    • /
    • 2016
  • This paper is the forth investigation on the evaluation methods of flow characteristics in a steady flow bench. In the previous works, it was concluded that the assumption of the solid rotation might cause serious problems and both of the eccentricity and the velocity profile distort the flow characteristics when using the ISM at 1.75B plane. Also particle image velocimetry (PIV) measurement at this position showed that the real velocity profile was far from the assumption of ISM evaluation. In this paper, the planar velocity profiles were measure from 1.75B to 6.00B position by PIV and the characteristics were examined according to the valve angles and lifts for further investigations about the effect of the position on the velocity profile. The results show that $26^{\circ}$ valve angle is always an unique exceptional case in all aspects. If the valve angle is $21^{\circ}$ and below, the planar velocity profiles according to the lift and the position are similar to each other, however, the tangential velocity curves along with the radial direction have common tendencies up to $16^{\circ}$ angle. Also the well arranged swirl behaviors are generally observed at the position above 3.00B and the velocity contour lines come closer to the concentric circle as the valve lift increases. In addition, the gradient of tangential velocity along with the radial direction from the swirl center becomes stable and constant as the position goes downstream. Concurrently the velocity gradient is larger to the eccentric direction of the center. In the meantime the tangential velocity curves along with the radial direction are irregular and various at 1.75B, however, they become regular and reach higher level as the evaluation position goes downstream. At this time the curves of 4.50B are the best fitted to the ideal one. On the other hand in an exceptional case, $26^{\circ}$, the velocity contours are very complicated over 6mm valve lift regardless the position and the gradient increases to the opposite direction of the eccentric center. Also, 6.00B is a best fitting position in the geometrical cylinder center base. With respect to the swirl center, the distribution range of centers for 1.75B is different to that for the other positions and the eccentricities of this plane are larger regardless the valve angle. After 1.75B, there is no certain tendency in the center position change according to the valve angle and lift. Additionally, the eccentricities are not sufficiently small to neglecting the effect on ISM measurement.

헬리컬 노즐의 피치각에 따른 볼텍스 튜브의 성능특성에 관한 연구 (A Numerical Study on the Effect of Pitch Angle of Helical Nozzle on the Vortex Tube Performance Characteristics)

  • 오영택;김귀순
    • 한국유체기계학회 논문집
    • /
    • 제19권1호
    • /
    • pp.11-17
    • /
    • 2016
  • In this paper, a numerical analysis was performed to investigate the effect of the pitch angle of a helical nozzle on the performance characteristics of a vortex tube. Three-dimensional numerical simulation has been performed with standard $k-{\varepsilon}$ turbulence model by using FLUENT 13.0. The effect of the pitch angle of helical nozzle was described in term of ${\beta}$. A CFD analysis was performed on ${\beta}=0^{\circ}$, $5^{\circ}$, $10^{\circ}$, $15^{\circ}$. In order to realize the influence of ${\beta}$ on performances of the vortex tube. Computation results were expressed by the ${\beta}-{\Delta}T_{h,c}$ graph and radial profiles of axial velocity and swirl velocity. The results showed that ${\beta}$ which improves energy separation capacity of vortex tube was $5^{\circ}$ at ${\alpha}=0.33$, 0.5 and $10^{\circ}$ at ${\alpha}=0.33$. Besides, It was confirmed that the results were closely related to axial velocity and swirl velocity.

여성 노인의 자세 정렬과 시공간 보행 변수 사이의 연관성 (Relationship Between the Postural Alignments and Spatio-temporal Gait Parameters in Elderly Woman)

  • 김성현;신호진;서혜림;정경심;조휘영
    • 대한물리의학회지
    • /
    • 제15권3호
    • /
    • pp.117-125
    • /
    • 2020
  • PURPOSE: Aging causes changes in the postural alignment and gait due to changes in the nervous and musculoskeletal systems. On the other hand, the relationship between the changes in posture alignment and gait is unclear. This study examined the relationship between the postural alignment and spatiotemporal gait parameters in Korean elderly women. METHODS: Thirty-two-healthy elderly women participated in this study. All subjects were assessed for their posture alignment and gait ability. Stepwise multiple linear regression was performed to determine to what extent the postural alignments could explain the spatiotemporal gait parameters. RESULTS: Coronal head angle was moderately correlated with the velocity (r = -.51), normalized velocity (r = -.46) and gait-stability ratio (r = .58) (p < .05). The trunk angle was moderately correlated with the normalized velocity (r = -.32) and gait-stability ratio (r = .32) and weakly correlated with the velocity (r = -.28) (p < .05). The coronal shoulder angle was moderately correlated with the swing phase (r = -.57), stance phase (r = .56), single limb stance (r = -.56) and double limb stance (r = .51) (p < .05). The coronal head angle and trunk angle accounted for 36% of the variance in velocity, 33% variance in normalized velocity and 46% variance in the gait-stability ratio (p < .05). The coronal shoulder angle accounted for 32% variance in the swing phase, 32% variance in the stance phase, 31% variance in the single limb stance and 26% variance in the double limb stance (p < .05). CONCLUSION: Changes in posture alignment in elderly women may serve as a biomarker to predict a decrease in walking ability due to physical aging.

배관구조에 따른 속도분포 변형과 선회가 오리피스 유량계의 압력차에 미치는 영향에 대한 수치적 연구 (Numerical Study on the Effects of Velocity Profile Distortion and Swirl on Pressure Difference of Orifice Flowmeter Due to Pipe structure)

  • 김홍민;허재영;김광용
    • 대한기계학회논문집B
    • /
    • 제27권10호
    • /
    • pp.1450-1456
    • /
    • 2003
  • Three-dimensional pipe flows with elbows, tees and headers in three different pipe systems are calculated to estimate the effect of asymmetry of axial velocity profile and swirl on measuring accuracy of an orifice flowmeter. It is evaluated how the pressure difference across the orifice is dependent on the upstream straight pipe length and how swirl intensity, swirl angle, and axial velocity distribution affect the measuring error of the orifice flowmeter. From the results, it is found that variation of the pressure difference across the orifice is negligible in case that maximum swirl angle is less than 2$^{\circ}$, and also that the pressure difference across the orifice is more sensitive to the asymmetry of axial velocity profile rather than the swirl intensity.

뒤 공중 돌기 유형에 따른 착지동작의 성공요인 분석 (Analysis of Successful Landing by the Type of the Salto Backward)

  • 한윤수
    • 한국운동역학회지
    • /
    • 제14권1호
    • /
    • pp.1-12
    • /
    • 2004
  • The purpose of this study is to provide training materials for practical use by investigating the kinematical variables of the successful landing by the type of the salto backward such as Tuck, Pike. For this study, the subjects are 4 male national gymnasts using 3-dimensional cinematographic method. Based on the results of this study, the conclusions are drawn as follows. 1. In flight phase, Tuck and Pike show fast extension after completing minimum angle of hip joint passing through the peak. It is very important factor to control body with gaining time before landing while decreasing the velocity of flight rotaion. 2. In Landing phase, the angles of each joint for successful landing are shown as $92deg{\sim}100deg$ for knee angle, $52deg{\sim}57deg$ for hip angle, and $56deg{\sim}70deg$ for shoulder angle. 3. Tuck and Pike dramatically decrease the height of COG, and horizontal/vertical velocity of COG from TD to LD. Also, it is shown that the knee angle, the hip angle and the shoulder angle decrease drastically. On the other hand, the angular velocity of trunk rotation shows negative direction and due to this, the angle of trunk rotation is shown as re-flexion.