• Title/Summary/Keyword: front pressure effect

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Effect of the Configuration of Plasma Jet Plug on Combustion Characteristics in a Constant Volume Vessel (플라즈마 제트 플러그의 형상이 정적연소기내 연소특성에 미치는 영향)

  • Kim, Munheon;Yoo, Hoseon;Oh, Byungjin;Park, Jungseo
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.23 no.5
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    • pp.593-602
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    • 1999
  • This paper presents combustion characteristics of LPG-air mixture ignited by the plasma jet in a cylindrical vessel with constant volume, in which our focus is placed on the multi-hole plug configuration. Four types of the plug configuration depending on the number of orifice and the arranged angle are considered, along with two cases of conventional spark ignition for comparison. Not only the flame propagation is photographed at intervals, but the pressure in the combustion chamber is also recorded through the entire combustion process. The results show that the plasma jet ignition enhances the overall combustion rate remarkably in comparison to the spark ignition by generating irregular flame front and penetrating through the unburned mixture. The combustion enhancement rate agrees favorably with the available data, which supports the validity of our experiment. Synthetically estimating, the two-hole sixty-degree plug appears to be the most desirable, in that the maximum pressure as well as the combustion duration is less affected by the sub-energy level than the others. It is also deduced that there may exist an optimal plug configuration capable of rapid combustion for a specific combustion chamber.

Study on Analytic of Opening Angles for Muffler Variable Valve of Automobile (자동차 머플러 내의 가변밸브의 열림 각에 관한 해석적 연구)

  • Park, Chungyeol;Kim, Kwonse;Kim, Jongil;Choi, Dooseuk
    • Transactions of the Korean Society of Automotive Engineers
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    • v.22 no.2
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    • pp.190-196
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    • 2014
  • Exhaust system by reinforcement of environment regulation came to the foe study necessity. And Exhaust system has necessary to increase the engine performance and silence. From this cause, Automobile has significantly considered production expense. this study makes process for checking the characteristics about Exhaust variable valve within muffler. Variable valve might reduce the baffle within muffler, It was possible to remove the front muffler. Therefor, To miniaturize a size of muffler might be increased by performance through cost-cutting effect and controling of back pressure. Because the Study on Variable valve installed within muffler, to measure the real data was hardly resulted one of the assignments. From manufactured conduct device, might measure data one of piece which was up-graded of problem. Considering to these point, stressed pressure distribution has analyzed on cross section, floating characteristics about velocity distribution around variable valve using analysis as computational fluid dynamics of Ansys with completed measurement data.

Numerical and Experimental Verification of Stress Wave Control Effect in SHPB Experiment using Pulse Shaper (Pulse Shaper를 이용한 SHPB 실험 응력파 제어 효과의 해석 및 실험적 검증)

  • Kim, Y.H.;Woo, M.A.;Kang, B.S.;Kim, J.
    • Transactions of Materials Processing
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    • v.26 no.5
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    • pp.314-322
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    • 2017
  • In the high-speed forming analysis, dynamic material properties considering a high strain rate are required. The split Hopkinson pressure bar (SHPB) experiment was performed for measuring dynamic material properties under high strain rate. The pulse shaping method was used to improve the accuracy of the SHPB experiment. A pulse shaper attached to the front of the incident bar was used for specimen dynamic stress equilibrium through stress wave control. Numerical analysis and SHPB test were performed to verify whether the pulse shaper affects the dynamic stress equilibrium in copper and Al6061 specimens. The results of SHPB test and numerical analysis show that the pulse shaper contributes to the dynamic stress equilibrium. Based on the improved stress equilibrium using a pulse shaper, the flow stress curves for copper and Al6061 materials were obtained at strain rates of 1344.4/sec and 1291.6/sec, respectively.

Study of Shock Tube for Wave Phenomenon in High Speed Railway Tunnel(II)-attenuation and Nonlinear Effect of Compression Waves- (고속철도 터널에서 발생하는 파동현상에 관한 충격파관의 연구(2)-압축파의 감쇠와 비선형효과-)

  • ;;Matsuo, Kazuyasu
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.19 no.8
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    • pp.1972-1981
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    • 1995
  • As a railway train enters a tunnel at high speed, a compression wave is formed in front of the train and propagates along the tunnel. The compression wave subsequently emerges from the exit of the tunnel, which causes an impulsive noise. The impulsive noise is closely related to the pressure gradient of the compression wave propagating the tunnel. In order to investigate the characteristics of the compression waves, in the present study an experiment was made using a shock tube. The results show that the strength of a compression wave decreases with the distance from the tunnel entrance and the nonlinear effect of compression wave appears to be significant if strength of the initial compression wave is greater than 7 kPa. Furthermore if the wave pattern is known, attenuation of the compression wave propagating in a tunnel can be reasonably predicted by a theoretical equation considering viscous action and heat transfer in boundary layer.

A Study on the Flying Characteristics of Zero-Load Sliders (제로-로드 슬라이더의 부상특성에 관한 연구)

  • 윤상준;강태식;최동훈
    • Tribology and Lubricants
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    • v.11 no.2
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    • pp.15-23
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    • 1995
  • A zero-load slider is composed of two outside rails which produce a lift force pushing up the slider from the disk surface and a wide reverse step region which produces a suction force attracting the slider to the disk surface. In this paper, the flying characteristics of zero-load sliders are obtained by using an optimization technique. In the pressure calculation module, the FIFD scheme is used to solve the modified Reynolds equation. The BFGS method and a line search algorithm is employed to predict the static flying attitude. To investigate the effect of the geometric- parameters of zero-load sliders on the flying characteristics, recess depth, front step width, rail width, and taper height are varied and the corresponding flying attitudes are obtained. Simulation results demonstrate that recess depth and rail width have significant influences on the flying characteristics.

Estimation of RPS Method Using 3-Dimensional Numerical Analysis (3차원 수치해석을 이용한 RPS 공법의 적용성 평가)

  • Roh, Jeong-Min;Shin, Eun-Chul
    • Journal of the Korean Society for Railway
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    • v.9 no.2 s.33
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    • pp.174-179
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    • 2006
  • Recently, the crossing tunnel has been constructed frequently to connect the separated area by highway and railroad. The construction of crossing tunnel must be progressed while maintaining the existing traffic of the highway as well as railroad. There are many cross funnelling methods such as NTR, TRCM, Messer Shield, Front Jacking, and Pipe Roof Method. The advantages of adopting RPS(Roof Panel Shield) method in crossing tunnel construction with comparing other existing cross funnelling methods are needed a little volume of concrete and easy to change the direction of cutting shoe during the construction of pipe roof, The 3-dimensional numerical analysis of RPS to consider the arching effect was performed for the application in the crossing tunnel under railroad. The earth pressure distribution and settlement were predicted when the RPS method was applied during the excavation for crossing railroad tunnel construction.

Effects of Material Position on Postural Stability during Manual Material Handling Tasks (인력물자취급작업시 작업 대상물의 위치가 신체자세동요에 미치는 영향)

  • Park, Jae-Gyu;Park, Seong-Ha
    • Journal of the Ergonomics Society of Korea
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    • v.23 no.4
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    • pp.1-8
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    • 2004
  • The objective of this study is to identify the effects of material position and physical fatigue on postural stability. Ten male subjects participated in this study. After bicycling exercises, their centers of pressure (COPs) were measured under four material handling positions and four excercise levels. The measured COPs were then utilized to calculate postural sway length in each experimental condition. Subjects' postural stability was quantified using the sway length. Results showed that the effect of different material handling position was significant on the postural sway length in both the posterior-anterior axis and the medio-lateral axis. Results also showed that the postural sway length was increased as physical fatigue accumulated, significantly in subject's posterior-anterior axis. The results imply that bearing a material on the back or front with both hands appeared to cause least sway length and instability.

Numerical Study on The Injection-Compression Molding Characteristic of High Viscosity Plastic Fluids (고점도 유동장이 사출-압축 성형에 미치는 영향)

  • Park, Gyun-Myoung;Kim, Chung-Kyun
    • Tribology and Lubricants
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    • v.18 no.5
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    • pp.345-350
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    • 2002
  • Recently, as the development of manufacturing technique on SMC(sheet molding compound), various numerical and experimental approaches to injection and compression molding have been investigated. Injection and compression molding, however, has so various cases with complicated boundary condition that it is difficult to analyze mold characteristics precisely. In addition, since a slight change in process variables can significantly change the resulting mold thickness, a proper design is important to compression molding process. Therefore, in this study, the effects of various parameters on compression molding process have been investigated using FEM(finite element method) to formulate the melt front advancement during the mold filling process. To verify the results of present analysis, they are compared with those of reference. The results show a strong effect of initial charge volume, injection time and pressure as a result of variations in the rectangular charge shape.

A Computational Study of the Supersonic Cavity Flow (초음속 Cavity 유동에 관한 수치해석적 연구)

  • Jung Sung-Jae;Gwak Jong-Ho;Kim Heuy-Dong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2004.10a
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    • pp.23-26
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    • 2004
  • A computational analysis has been conducted to investigate the detailed flow structure inside a supersonic cavity. The free stream Mach number and Reynolds number are 1.83 and $6.02\times10^5$ respectively. In the present study, the depth and width of the cavity are changed to investigate the effect of the cavity dimensions. A fully implicit finite volume scheme is applied to solve the three-dimensional, steady, unsteady, compressible, Navier-Stokes equations. The computed results are validated with the previous experimental data available. The present computation provides reasonable predictions of the cavity flow, compared with experimental results. The obtained results show that a shock wave is generated in front of the downstream edge of the cavity and the dominant frequencies of the pressure oscillations inside the cavity were obtained.

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3D-Numerical Simulation of Wave Pressure Acting on Caisson and Wave Characteristics near Tip of Composite Breakwater (혼성방파제의 케이슨에 작용하는 파압과 선단 주변에서 파랑특성에 관한 3차원수치시뮬레이션)

  • Choi, Goon-Ho;Jun, Jae-Hyoung;Lee, Kwang-Ho;Kim, Do-Sam
    • Journal of Korean Society of Coastal and Ocean Engineers
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    • v.32 no.3
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    • pp.180-201
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    • 2020
  • It has been widely known that the effect of diffracted waves at the tip of composite breakwater with finite length causes the change of standing wave height along the length of breakwater, the spatial change of wave pressure on caisson, and the occurrence of meandering damage on the different sliding distance in sequence. It is hard to deal with the spatial change of wave force on trunk of breakwater through the two-dimensional experiment and/or numerical analysis. In this study, two and three-dimensional numerical techniques with olaFlow model are used to approach the spatial change of wave force including the impulsive breaking wave pressure applied to trunk of breakwater, the effect of rear region, and the occurrence of diffracted waves at the tip of caisson located on the high crested rubble mound. In addition, it is thoroughly studied the mean wave height, mean horizontal velocity, and mean turbulent kinetic energy through the numerical analysis. In conclusion, it is confirmed that the larger wave pressure occurs at the front wall of caisson around the still water level than the original design conditions when it generates the shock-crushing wave pressure checked by not two-dimensional analysis, but three-dimensional analysis through the change of wave pressure applied to the caisson along the length of breakwater.