• 제목/요약/키워드: Static pressure

검색결과 1,377건 처리시간 0.023초

혼화 및 유동특성에 미치는 라인믹서 내 혼합요소의 영향 (Effect of Mixing Elements in Line Mixer on Mixing and Flow Characteristics)

  • 유대겸;이계복
    • 한국산학기술학회논문지
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    • 제19권10호
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    • pp.437-443
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    • 2018
  • 본 연구에서는 라인믹서 내의 압력손실과 혼화성능에 대한 혼합요소의 영향을 해석하였다. 기체와 액체가 혼합된 고농도 오존수 장치는 단체급식시설의 살균 및 소독, 양식장의 수질관리 등 다양한 분야에서 사용되고 있다. 그러나 기존에 사용되는 장치는 가압방식을 사용하여 부피가 매우 크다. 최근에는 기후 변화로 강수량이 감소하여 지하수 및 지표수의 오염으로 음용수의 살균은 매우 중요하다. 따라서 기존의 장치와 대비하여 작은 공간을 사용하면서도 정수기능을 갖는 라인믹서형 기체-액체 혼합장치의 개발이 필요하다. 본 연구에서는 라인믹서 장치 내에 삽입한 혼합요소인 static mixer의 개수, 오리피스의 형태와 개수, 오리피스에 부착된 베인의 모양에 따른 유입유체의 혼화상태와 유동특성을 전산유체역학 모사를 통해 해석하고 혼화상태에 미치는 영향을 평가하였다. 곡면의 베인을 부착한 오리피스를 라인믹서에 사용한 경우 static mixer를 사용한 경우와 비교하여 비슷한 혼화정도를 나타내면서 압력손실양은 50% 이상 감소하는 것을 확인하였다.

흡음형 디퓨저 소음기의 성능 (Performance of Absorption Diffuser Silencers)

  • 정갑철;현승일;이종우;권영필
    • 소음진동
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    • 제4권3호
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    • pp.377-384
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    • 1994
  • This paper is an investigation of the performance of absorption diffusers to suppress the vent noise emitted when high pressure gas is throttled. First, experiment for the static performance is carried out. When there is no through-flow, the insertion loss has been obtained in terms of 1/3 octave band spectrum and the effect of the number of diffusers and the thickness of the absorption material on the static performance has been obtained. And the similarity in the spectrum of the static insertion loss is confirmed by comparing two similar models with different size. Second, the dynamic performance has been obtained by experiment using blow-down of compressed air from a storage tank through an orifice of diameter 10 mm. The back pressure by the diffuser is measured and compared with that of a single diffuser. It is found that the insertion loss of asingle diffuser is very low around 3 dB at high frequencies with negative value at low frequencies. By absorption material between the diffuser tubes, however, the performance is increased considerably. Without flow the static insertion loss increases by 3 - 4 dB by doubling the thickness or the density of the absorptionmaterial. With flow, however, the dynamic insertion loss increases. While, the back pressure by the diffuser is small enough to be neglected.

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Aerodynamic forces on fixed and rotating plates

  • Martinez-Vazquez, P.;Baker, C.J.;Sterling, M.;Quinn, A.;Richards, P.J.
    • Wind and Structures
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    • 제13권2호
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    • pp.127-144
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    • 2010
  • Pressure measurements on static and autorotating flat plates have been recently reported by Lin et al. (2006), Holmes, et al. (2006), and Richards, et al. (2008), amongst others. In general, the variation of the normal force with respect to the angle of attack appears to stall in the mid attack angle range with a large scale separation in the wake. To date however, no surface pressures have been measured on auto-rotating plates that are typical of a certain class of debris. This paper presents the results of an experiment to measure the aerodynamic forces on a flat plate held stationary at different angles to the flow and allowing the plate to auto-rotate. The forces were determined through the measurement of differential pressures on either side of the plate with internally mounted pressure transducers and data logging systems. Results are presented for surface pressure distributions and overall integrated forces and moments on the plates in coefficient form. Computed static force coefficients show the stall effect at the mid range angle of attack and some variation for different Reynolds numbers. Normal forces determined from autorotational experiments are higher than the static values at most pitch angles over a cycle. The resulting moment coefficient does not compare well with current analytical formulations which suggest the existence of a flow mechanism that cannot be completely described through static tests.

소형항공기용 왕복엔진의 정적 성능시험 연구 (A Study on the Static Performance Test of a Reciprocating Engine for Small Aircraft)

  • 김근배;안석민;김근택;최선우
    • 한국추진공학회지
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    • 제7권3호
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    • pp.53-60
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    • 2003
  • 한국항공우주연구원에서 개발 중인 소형항공기와 관련하여 지상에서 왕복엔진의 정적 성능을 측정하기 위한 시험장치를 개발하였다. 시험장치는 Pusher형 추진시스템을 장착하고 구동하는 장치와 엔진의 기본적인 작동 감시 및 엔진 토크와 프로펠러 추력을 비롯한 여러 성능 변수들을 측정하고 처리하는 데이터 획득 장치로 구성되었다 먼저 기본 작동시험에서 도출된 성능데이터를 원래 엔진데이터와 비교 분석하여 시험장치의 기능을 검증하였다. 성능시험은 3단계에 걸쳐 다양한 시험조건에서 수행되었으며, 엔진의 흡기압력과 토크, 배압, 연료유량, 그리고 프로펠러의 정지추력을 측정하고 분석하였다.

Comparison of Effects on Static Balance in Stroke Patients According to Visual Biofeedback Methods

  • Kyu-Seong Choi;Il-Ho Kwon;Won-Seob Shin
    • Physical Therapy Rehabilitation Science
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    • 제12권3호
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    • pp.320-326
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    • 2023
  • Objective: The purpose of this study is to investigate the impact of visual biofeedback methods utilizing pressure sensors on the static balance of stroke patients. Design: Randomized crossover study. Methods: A total of 27 patients with hemiparesis participated in this study. The following three feedback conditions were considered: condition 1 (Knowledge of performance feedback), condition 2 (Knowledge of result feedback), and condition 3 (None feedback). A force plate was used to measure static balance. The total sway length, average sway velocity, x-axis excursion, and y-axis excursion of the center of pressure were measured. One-way repeated-measures analysis of variance was employed for comparisons of variables between each condition. The statistical significance level was set at α = 0.05 for all analyses. Results: There was a significant difference in the static balance results between each feedback condition (p<0.05). In the post-hoc results, it was confirmed that the static balance was significant in the order of knowledge of performance feedback, knowledge of result feedback, and none feedback. Conclusions: When comparing the three conditions, it was observed that knowledge of performance feedback showed the most improved effect on static balance ability. As further research progresses, that this approach could be used as an effective intervention method in clinical settings.

하퇴 의지 사용자의 족저압 분포 특성에 관한 연구 (A Study of Characteristics of Foot Pressure Distribution in Trans-tibial Amputee Subjects)

  • 김장환;신헌석
    • 한국전문물리치료학회지
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    • 제8권3호
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    • pp.1-10
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    • 2001
  • The purpose of this study was to compare the static pressure, dynamic pressure, dynamic pressure-time integral, relative impulse, and contact time between the sound lower limb and amputated lower limb in trans-tibial amputee subjects using Parotec system. Seventeen trans-tibial amputee subjects wearing endoskeletal trans-tibial prosthesis voluntarily participated in this study. The results were as follows: 1) In static standing condition, there were significantly higher static pressure in sound lower limb insole sensor of 10, 14, 15, 18, 19, 23, and 24 and in amputated lower limb insole sensor of 9, 12, and 16 (p<.05). 2) In dynamic gait condition, there were significantly higher dynamic pressure in sound lower limb insole sensor of 2, 18, 22, 23, and 24 and in amputated lower limb insole sensor of 5, 9, 10, 11, 12, 14, 15, and 16 (p<.05). 3) In dynamic gait condition, there were significantly higher pressure-time integral in sound lower limb insole sensor of 2, 4, 18, 19, 20, 21, 23, and 24 and in amputated lower limb insole sensor of 5, 11, 12, and 15 (p<.05). 4) In dynamic gait condition, there were significantly higher relative impulse in sound lower limb insole sensor of 18, 19, 20, 22, 23, and 24 and in amputated lower limb insole sensor of 5, 9, 10, 11, 12, and 15 (p<.05). 5) In dynamic gait condition, there was significantly higher percentage of contact time in push off phase of sound lower limb and in support phase of amputated lower limb (p<.05). These results suggest that trans-tibial amputee subjects had characteristics of shortened push off phase due to unutilized forefoot and of lengthened support phase with higher pressure in the midfoot.

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5공 압력프로브의 측정에 의한 Gun식 가스버너의 스월유동장 고찰 (Investigation of the Swirling Flow Fields of a Gun-Type Gas Burner by the Measurement of a Five-Hole Pressure Probe)

  • 김장권;오석형
    • 동력기계공학회지
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    • 제19권1호
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    • pp.19-23
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    • 2015
  • The swirling flow fields of a gun-type gas burner(GTGB) without a combustion chamber were measured by a straight-type five-hole pressure probe(FHPP) under the cold flow condition. The three kinds of velocity components and the static pressure were calculated by using a non-nulling calibration method covering the velocity reduction performance of the effective flow attack angle of ${\pm}80^{\circ}$. As a result, the velocity and static pressure measured by a FHPP comparatively shows the better performance on the swirling flow of a GTGB than those measured by X-probe.

Pseudo-dynamic approach of seismic earth pressure behind cantilever retaining wall with inclined backfill surface

  • Giri, Debabrata
    • Geomechanics and Engineering
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    • 제3권4호
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    • pp.255-266
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    • 2011
  • Knowledge of seismic earth pressure against rigid retaining wall is very important. Mononobe-Okabe method is commonly used, which considers pseudo-static approach. In this paper, the pseudo-dynamic method is used to compute the distribution of seismic earth pressure on a rigid cantilever retaining wall supporting dry cohesionless backfill. Planar rupture surface is considered in the analysis. Effect of various parameters like wall friction angle, soil friction angle, shear wave velocity, primary wave velocity, horizontal and vertical seismic accelerations on seismic earth pressure have been studied. Results are presented in terms of tabular and graphical non-dimensional form.

초음속 동축 제트의 구조에 미치는 외부노즐 분사각의 영향 (Effect of Outer Nozzle Ejection Angle on Jet Structure issuing from Supersonic Dual Coaxial Nozzle)

  • 백승철;권수영;주성열;권순범
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 추계학술대회논문집B
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    • pp.426-431
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    • 2001
  • This paper experimentally investigates the characteristics of dual coaxial jet issuing from inner supersonic nozzle and four kinds of outer converging nozzle of 40, 50, $60^{\circ}$ and $70^{\circ}$ in outer ejection angle. The pressure ratio of the stagnation to the exit ambient pressures in the inner supersonic nozzle of constant expansion rate is 7.5, which is corresponded to the condition of a slightly underexpanded, and that of outer nozzle is 4.0. Flow visualizations by using of shadowgraph method, impact pressure and centerline static pressure measurements are presented. It is found that the jet structure is changed significantly by the variation of outer nozzle ejection angle. Impact pressure level is lower and undulation of static pressure is higher, as the injection angle of outer jet increases.

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비소음 측정을 이용한 저소음 축류홴 설계 (Design of Low Noise Axial Flow Fan Using Specific Sound Presssure Level)

  • 김창준;이동익
    • 소음진동
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    • 제10권5호
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    • pp.873-879
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    • 2000
  • Experimental investigation was conducted to study the effects of pitch angle maximum camber on the performance and noise of an axial-flow fan used in outdoor-unit of air -conditioner. For this study the axial-flow fan whose pitch angle can be varied was made and the Specific sound Pressure Level and other coefficients were measured using the anechoic fan tester. It is found that pitch angle affects more severly than the maximum camber on the fan performance. On the while the maximum camber affects much on the specific sound power level. Present results show that it is important to choose the optimum pitch angle and maximum camber to design the high-performance and low-noise axial-flow fan and specific noise measured in the anechoic fan tester can be sued effectively for the design of low-noise fan.

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