• Title/Summary/Keyword: Steady Performance

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Effects of Warm-up Performance on SI Engine with Exhaust Heat Recovery System (배기열 회수장치 적용에 따른 SI 엔진의 웜업 성능에 미치는 영향)

  • Park, Kyoun-Suk;Suh, Ho-Cheol;Park, Sun-Hong;Kim, In-Tae;Jang, Sung-Wook
    • Transactions of the Korean Society of Automotive Engineers
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    • v.19 no.6
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    • pp.53-60
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    • 2011
  • The effect of exhaust heat recovery system can be evaluated by two well known method. First method is to measure the time duration from engine start under cold coolant temperature till coolant get warmed. By this methodology coolant warming duration can be index of warm-up effect. Second method is to analyze heat balance of the engine during warm-up phase under steady engine operation so that wasted energy by losses such as cooling and exhaust can be index of warm-up effect. This study focused on evaluation of warming-up effect by both methodology above mentioned using 2L SI engine under from idle to 2000rpm steady condition. Results, idle operation showed low heat recovery efficiency but under higher engine speed condition, remarkable heat recovery efficiency improvement was observed. In 2000rpm steady condition, warm-up duration of engine is decreased by exhaust heat recovery system.

Numerical simulation of unsteady propeller force for a submarine in straight ahead sailing and steady diving maneuver

  • Pan, Yu-cun;Zhang, Huai-xin;Zhou, Qi-dou
    • International Journal of Naval Architecture and Ocean Engineering
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    • v.11 no.2
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    • pp.899-913
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    • 2019
  • In order to provide a complementary perspective to the effects of the maneuvering motions on the unsteady propeller performance, the numerical simulation of the flow field of the hull-rudder- propeller system is performed by Unsteady Reynolds-averaged Naiver-Stokes (URANS) method. Firstly, the flow fields around the submarine model without the presence of propeller in straight ahead motion and the steady diving maneuvers with submergence rudder deflections of 4°, 8° and 12° are predicted numerically. The non-uniformity characteristic of the nominal wake field is exacerbated with the increase submergence rudder angle. Then the flow field around the SUBOFF-G submarine fitted with the 4381 propeller is simulated. The axial, transverse and vertical unsteady propeller forces in different maneuvering conditions are compared. In general, as the submarine maneuvers more violently, the harmonic amplitudes of the unsteady force at the 2BPF and 3BPF increased more significantly than that at BPF.

Analysis of Steady Heat Conduction for Rubber Pads of a Tank Track Subjected to Dynamic Loading (동적하중을 받는 궤도차량 고무패드의 정상 열전도 해석)

  • Kim, Hyung-Je;Kim, Byung-Tak
    • Elastomers and Composites
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    • v.36 no.3
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    • pp.153-161
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    • 2001
  • The rubber pads era tank which undergo dynamic deformations with the sufficient amplitudes and frequencies lead to a considerable internal temperature rise due to the heat generation. The heat generation which is dependent on the viscoelastic characteristics or a rubber is due to the conversion of partial mechanical energy into thermal energy identical to the area oi hysteresis loop. Heat generation without adequate heat dissipation leads to heat build-up and the excessive temperature rite exerts a bad influence upon the performance and the life of rubber products. In this paper, temperature distributions of the rubber pads of a tank track subjected to dynamic loads are obtained under the assumption of the steady state. Heat generation rates used in this finite element analysis are acquired through experiments and the computed temperature fields are displayed in isothermal contour regions.

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Enhancement of Airfoil Post-Stall Characteristics via a Jet Blowing (제트 블로잉에 의한 에어포일의 실속후 특성 향상)

  • Lee, Ki-Young;Chung, Heong-Seok;Cho, Dong-Hyun;Sohn, Myong-Hwan
    • Journal of the Korea Institute of Military Science and Technology
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    • v.10 no.2
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    • pp.188-197
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    • 2007
  • Active flow control, in the form of steady and unsteady momentum injection via jet blowing was studied. A jet was obtained by pressing a plenum inside the airfoil and ejecting flow out of a thin slot. The normal and drag forces were measured with leading edge or trailing edge blowing Jet and compared with the results obtained with no blowing. The blowing jet has been shown to improve the aerodynamic performance of the airfoil. The steady jet proved more effective than pulsating jet in these experimental conditions. Furthermore for the case of leading edge steady blowing jet, the alleviation of non-linearity in the normal force curve slope can be seen at higher angles of attack. No effective trailing edge jet was observed in this highly separated flow. This shows that the stall control is highly depends on the characteristics of the boundary layer near the jet slot.

Hydraulic Shock Load Response of Activated Sludge Process (활성슬러지공정의 수리학적 충격부하 반응)

  • Whang, Gye Dae;Kim, Min Ho;Ko, Sae;Cho, Chul Hwi
    • Journal of Korean Society of Water and Wastewater
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    • v.11 no.3
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    • pp.67-78
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    • 1997
  • The objective of study was to examine to transient response of hydraulic shock loading in activated sludge process for treatment of municipal sewage. The general experiment approach was to operate the system under steady-state(pre-shock), then to apply step changes during 24hours in fourfold hydraulic shock loading at the same organic loading. Performance was assessed in both the transient state and the new steady-state(post-shock). Three bench scale activated sludge reactors were operated to investigate the effect of fourfold hydraulic shock loading on TSS and COD removal efficiency. In activated sludge reactors operated with 13hours and 7hours of HRT, effluent quality of all reactors was not changed for few effects, and also showed no foaming and no sludge bulking. Those results are the same as sludge withdrawn reactors. The effect of fourfold hydraulic shock loading on the activated sludge reactors operated with 3hours of HRT was most severe. The effluent quality was deteriorated significantly and generate foaming in reactors. Less than 24hours after the fourfold shock loading applied, the activated sludge system seemed to attain a new steady-state condition as show by effluent.

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Analysis of in-cylinder steady flow for dual-intake-valve gasoline engine using single-frame particle tracking velocimetry (단일 프레임 입자 추적법을 이용한 흡입 2밸브 가솔린 기관의 실린더 내 정상 유동 해석)

  • Lee, Chang-Sik;Lee, Gi-Hyeong;Im, Gyeong-Su;Jeon, Mun-Su
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.21 no.5
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    • pp.650-658
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    • 1997
  • Analysis and control of intake charge motion such as swirl and tumble are very important factors in improving the gasoline engine performance. In this paper, single-frame PTV (particle tracking velocimetry) is used to investigate intake tumble patterns in a steady flow test rig of gasoline engine with dual-intake-valve and pent-roof combustion chamber. Intake tumble pattern is quantified in accordance with blockage ratio of TIV (tumble intensifying valve) with single- frame PTv.The view of the instantaneous 2-D velocity field gives a realistic understanding of in-cylinder flow field. Thus it is confirmed that PTV is a effective tool in engine design. In conventional port, two tumble structures appear clearly, and the larger one is observed under the exhaust valve side and the smaller is right below the intake valve side. The larger vorticity is observed in TIV port, thus it is concluded that TIV have an effect on intensified tumble motion in cylinder flow.

Numerical Study on Steady and Unsteady Flow Characteristics of Nozzle-Rotor Flow in a Partial Admission Supersonic Axial Turbine with Sweep Angle (스윕 각이 적용된 부분 흡입형 초음속 축류 터빈의 정상, 비정상 공력 특성에 관한 수치적 연구)

  • Jeong, Soo-In;Kim, Kui-Soon
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2012.05a
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    • pp.173-179
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    • 2012
  • Steady and unsteady three-dimensional RANS simulations have been performed on partial admission supersonic axial turbine having backward/forward sweep angles(${\pm}15^{\circ}$) and the results are compared with each other. The objective of this paper is to study the effect of unsteadiness on turbine flow characteristics and performances. The all results indicated that the losses of unsteady simulations were greater than those of steady cases. It was also shown that BSW model give the effect on the reducing of mass flow rates of tip leakage. In unsteady simulation, the increase of t-to-s efficiency at Rotor Out plane was observed more clearly.

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Two-way fluid-structure interaction simulation for steady-state vibration of a slender rod using URANS and LES turbulence models

  • Nazari, Tooraj;Rabiee, Ataollah;Kazeminejad, Hossein
    • Nuclear Engineering and Technology
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    • v.51 no.2
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    • pp.573-578
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    • 2019
  • Anisotropic distribution of the turbulent kinetic energy and the near-field excitations are the main causes of the steady state Flow-Induced Vibration (FIV) which could lead to fretting wear damage in vertically arranged supported slender rods. In this article, a combined Computational Fluid Dynamics (CFD) and Computational Structural Mechanic (CSM) approach named two-way Fluid-Structure Interaction (FSI) is used to investigate the modal characteristics of a typical rod's vibration. Performance of an Unsteady Reynolds-Average Navier-Stokes (URANS) and Large Eddy Simulation (LES) turbulence models on asymmetric fluctuations of the flow field are investigated. Using the LES turbulence model, any large deformation damps into a weak oscillation which remains in the system. However, it is challenging to use LES in two-way FSI problems from fluid domain discretization point of view which is investigated in this article as the innovation. It is concluded that the near-wall meshes whiten the viscous sub-layer is of great importance to estimate the Root Mean Square (RMS) of FIV amplitude correctly as a significant fretting wear parameter otherwise it merely computes the frequency of FIV.

No Effect of Diltiazem on the Hepatic Clearance of Indocyanine Green in the Rats

  • Joo, Eun-Hee;Lee, Yong-Bok
    • Archives of Pharmacal Research
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    • v.21 no.4
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    • pp.411-417
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    • 1998
  • In order to investigate the effect of the pretreatment with various doses of diltiazem (DTZ) on the pharmacokinetics of indocyanine green (ICG) at steady state, especially the hepatic blood clearance due to the change of hepatic blood flow, the following experiments were carried out with ICG, a hepatic function test marker, not metabolized in liver and only excreted in bile. The intravenous bolus injection ($3,780\mu\textrm{g}$/kg) and the constant-rate infusion ($10,100\mu\textrm{g}$/kg/hr) of ICG into the left femoral vein were made in order to check the steady-state plasma concentration ($C_{ss} of $10\mu\textrm{g}$/ml) of ICG at 20, 25 and 30 min. Following a 90-min washout period, the intravenous bolus injection (108, 430, 860 and $1,720\mu\textrm{g}$/kg) and the constant-rate infusion (108, 433, 866 and $1,730\mu\textrm{g}$/kg/hr) of DTZ into the right femoral vein were made and the achievement of the steady-state plasma levels ($C_{ss} of 50, 200, 400 and 800 ng/ml) of DTZ were conformed at 60, 70 and 80 min. During the steady state of DTZ, the intravenous bolus injection ($3,780\mu\textrm{g}$/kg) and the constant-rate infusion ($10,200\mu\textrm{g}$/kg/hr) of ICG into the left femoral vein were made and also the steady-state plasma concentration of ICG was checked at 20, 25 and 30 min. The plasma concentrations of DTZ and ICG were determined using a high performance liquid chromatographic technique. At the steady state, the hepatic blood clearance of ICG was obtained from the plasma concentration and blood-to-plasma concentration ratio ($R_B$) of ICG. The pretreatment with various doses of DTZ did not influence the plasma concentrations, $R_B$ and plasma free fraction ($f_p$) of ICG. So the hepatic blood clearance of ICG was independent of concentration of DTZ. The hepatic blood clearance of ICG could be affected by both hepatic bood flow and hepatic intrinsic clearance. But there was no change of the hepatic blood clearance of ICG between the control and the DTZ-pretreated rats in this study. So it may be suggested that DTZ does not influence hepatic blood flow.

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Studies on the Steady State and Dynamic Characteristics of a Carbon Dioxide Air-Conditioning System for Vehicles (자동차용 이산화탄소 냉방 시스템의 정상상태 및 동적 특성에 관한 연구)

  • Park, Min-Su;Kim, Sung-Chul;Kim, Dal-Won;Kim, Min-Soo
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.31 no.6 s.261
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    • pp.531-538
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    • 2007
  • In this study, an air conditioning system using carbon dioxide as a refrigerant was developed for automotive cabin cooling. Experiments have been carried out to examine the steady state and dynamic characteristics of this system. The system consists of a compressor, a gas cooler, an evaporator, an expansion device, an internal heat exchanger and an accumulator. The compressor is a variable displacement type, driven by the electric motor, and the gas cooler and the evaporator are aluminum extruded heat exchangers of micro channel type. The $CO_2-refrigerant$ charge, the compressor speed, the air inlet temperature of the gas cooler, the air inlet temperature and the air flow rate of the evaporator and the cooling load are varied and the performance of the system is experimentally investigated. As the compressor speed increased, cooling capacity increased, but the coefficient of performance was deteriorated. As the cabin air temperature or the air flow rate to the cabin was set high, both the cooling capacity and the COP increased. In the cool down experiment with 1.0 or 2.0 kW of heat load, the dynamic characteristics of the air-conditioning system were investigated. For a given capacity of compressor, cool down speed was monitored, and the temperature change was acceptable fur low heat load condition.