• Title/Summary/Keyword: Pressure Loss Coefficient

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Development of Integrated HVAC Noise Analysis Program for Ships (선박용 통합 HVAC 소음해석 프로그램 개발)

  • Han, Ju-Bum;Hong, Suk-Yoon;Song, Jee-Hun;Kim, Nho-Seong;Chun, Seung-Hyun
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2011.04a
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    • pp.588-593
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    • 2011
  • The Main design parameters of ship HVAC systems are pressure drop and noise analysis of ducts. The Noise prediction for HVAC(Heating, Ventilating and Air Conditioning) systems are normally performed by empirical method suggested by NEBB(National Environmental Balancing Bureau, 1994), but NEBB's method is not suitable for the ship HVAC systems. In this paper, numerical analysis methods are used to develop a noise prediction method for the ship HVAC systems, especially for large ducts. To develop regression formula of attenuation of sound pressure level in large duct, Boundary Element Method(BEM) is used. Using dynamic loss coefficient which is suggested by ASHRAE fitting data base and numerical methods of HVAC noise analysis, integrated HVAC noise analysis of Program is developed. The developed program can present pressure drop and noise analysis of the ship HVAC systems. To verify the accuracy and convenience of the developed program, prediction of HVAC system for Semi-Submersible Drilling RIG is carried out and the results are compared with measurement of noise level during sea trial.

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High-pressure Air Impulse Technique for Rehabilitating Well and Its Application to a Riverbank Filtration Site in Korea

  • Jeon, Hang-Tak;Hamm, Se-Yeong;Cheong, Jae-Yeol;Han, Suk-Jong;Yun, Sul-Min
    • Journal of Environmental Science International
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    • v.28 no.10
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    • pp.887-898
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    • 2019
  • Rehabilitation work is required to increase well productivity, which decreases with the elapsed time of pumping owing to the clogging of the water well. Clogging causes not only a reduction in the well productivity but also a deterioration of the water quality. For unclogging and rehabilitating wells, several techniques are used such as brushing, air surging, surge blocks, and gas impulse. In this study, the high-pressure air impulse technique, which effectively and economically rehabilitates wells, was applied to a riverbank filtration site in Korea for the same objective. At most of the wells, the hydraulic parameters (transmissivity, storage coefficient, and specific capacity) were increased by the application of the high-pressure air impulse technique. The well loss change values also indicate an increase in the hydraulic parameters by the air impulse implementation. Thus, the high-pressure air impulse technique can be efficiently and economically applied to water and riverbank filtration wells for rehabilitating the decreased productivity.

Experimental Study on Pressure Loss of Flow Parallel to Rod Bundle with Spacer Grid (지지격자가 있는 봉다발과 축방향으로 평행한 유동의 압력손실에 관한 실험적 연구)

  • Lee, Chi-Young;Shin, Chang-Hwan;Park, Ju-Yong;In, Wang-Kee
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.36 no.7
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    • pp.689-695
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    • 2012
  • The friction factor in a rod bundle and the loss coefficient at a spacer grid were examined. As a test section, 25 smooth rods, 9.5 mm in diameter and 2000 mm in length, were prepared and installed in a $5{\times}5$ square array in a square channel. In this case, the P/D (Pitch-to-Diameter ratio) was 1.35. In this work, plain (i.e., no mixing vanes), split-vane, and hybrid-vane spacer grids were tested. In a bare rod bundle (i.e., no spacer grid), the measured friction factors were in good agreement with the previous correlations. Among the spacer grids tested, the hybrid-vane spacer grid presented the largest friction factor in the rod bundle and loss coefficient. This may be because of the flow pattern change induced by large relative plugging of the flow cross section and mixing vane geometry. At Re=$5{\times}10^5$, the predicted loss coefficients of plain, splitvane, and hybrid-vane spacer grids were approximately 0.79, 0.80, and 0.88, respectively.

The study of CFD Modelling and numerical analysis for MSW in MBT system (생활폐기물 전처리시스템(MBT)의 동역학적 수치해석 및 모델링에 대한 연구)

  • Lee, Keon joo;Cho, Min tae;Na, Kyung Deok
    • Journal of the Korea Organic Resources Recycling Association
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    • v.18 no.3
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    • pp.77-86
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    • 2010
  • In this study, the model of the indirect wind suction waste sorting machine for characteristics of the screening of waste was studied using computational fluid dynamics and the drag coefficient for the model and the suction wind speed were obtained. The wind separator are developing by installing a cyclone air outlet to the suction blower impeller waste is selective in a way that does not pass the features and characteristics of the inlet pipe of the pressure loss and separation efficiency can have a significant impact on. Using Wind separator for selection of waste in the waste prior research on the aerodynamic properties are essential. For plastic cases, it is reasonable to take the drag coefficient between 0.8 and 1.0, and for cans, compression depending on whether the cans, the drag coefficient is in the range from 0.2 to 0.7. The separation efficiency of waste as change suction speed was the highest efficiency when the suction speed was 25~26 m/s. Shape of the inlet, depending on how the transfer pipe of the duct pressure loss occurs because the inlet velocity changes through the appropriate design standards to allow for continued research is needed.

Effects of the design variables and their constraints on the stage performance of an axial flow turbine (축류 터빈의 설계 변수 및 설계 변수의 제한조건이 성능에 미치는 영향)

  • 박호동;정명균
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.15 no.6
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    • pp.2109-2124
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    • 1991
  • A simulation program is developed to analyse the performance of an axial flow turbine stage based on the meanline prediction method. The gradient projection method is utilized to minimize the aerodynamic losses under the specified constraints on such as flow coefficient, total pressure ratio, stage power and blade loading coefficient. After obtaining the optimum point for minimizing the stage loss, a sensitivity analysis is carried out ground the optimum point to find the effects of the design variables and the design constraints on the stage performance. The result of the senitivity analysis under a constant blade loading coefficient shows that the total loss is more sensitive to the mean diameter, the absolute flow angle at nozzle outlet, the relative flow angle at rotor outlet and the axial mean velocity compared to the chords and the pitches. Moreover, the design constraints on the degree of reaction at root and the blade length-to-diameter ratio are found to be most influencial on the maximization of the overall aerodynamic efficiency.

Performance Evaluation of Nano-Lubricants at Thrust Slide-Bearing of Scroll Compressor (나노 윤활유를 이용한 스크롤 압축기 스러스트 베어링의 윤활특성 평가)

  • Cho, Han-Jong;Cho, Yong-Il;Cho, Sang-Won;Lee, Jae-Keun;Park, Min-Chan;Kim, Dae-Jin;Lee, Kwang-Ho
    • Journal of the Korean Society for Precision Engineering
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    • v.29 no.1
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    • pp.121-125
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    • 2012
  • This paper presents the friction and anti-wear characteristics of nano-oil with a mixture of a refrigerant oil and carbon nano-particles in the thrust slide-bearing of scroll compressors. Frictional loss in the thrust slide-bearing occupies a large part of total mechanical loss in scroll compressors. The characteristics of friction and anti-wear using nano-oil is evaluated using the thrust bearing experimental apparatus for measuring friction surface temperature and the coefficient of friction at the thrust slide-bearing as a function of normal loads up to 4,000 N and rotating speed up to 3,200 rpm. It is found that the coefficient of friction increases with decreasing rotating speed and normal force. The friction coefficient of carbon nano-oil is 0.023, while that of pure oil is 0.03 under the conditions of refrigerant gas R-22 at the pressure of 5 bars. It is believed that carbon nano-particles can be coated on the friction surfaces and the interaction of nano-particles between surfaces can be improved the lubrication in the friction surfaces. Carbon nano-oil enhances the characteristics of the anti-wear and friction at the thrust slide-bearing of scroll compressors.

Performance Evaluation of Nano-Lubricants at Thrust Slide-Bearing of Scroll Compressors (나노 윤활유를 이용한 스크롤 압축기 스러스트 베어링의 윤활특성 평가)

  • Cho, Sang-Won;Kim, Hong-Seok;Ahn, Young-Chull;Lee, Jung-Eun;Lee, Jae-Keun;Lee, Hyeong-Kook;Lee, Byeong-Chul;Kim, Dong-Han;Park, Jin-Sung
    • Proceedings of the SAREK Conference
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    • 2006.06a
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    • pp.1219-1224
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    • 2006
  • This paper presents the friction and anti-wear characteristics of nano-oil with n mixture of a refrigerant oil and carbon nano-particles in the thrust slide-bearing of scroll compressors. Frictional loss in the thrust slide-bearing occupies a large part of total mechanical loss in scroll compressors. The characteristics of friction and anti-wear Lising nano-oil is evaluated using the thrust bearing tester for measuring friction surface temperature and the coefficient of friction at the thrust slide-bearing as a function of normal loads up to 4,000 N and orbiting speed up to 3,200 rpm. It is found that the coefficient of friction increases with decreasing orbiting speed and normal force. The friction coefficient of carbon nano-oil is 0.015, while that of pure oil is 0.023 under the conditions of refrigerant gas R-22 at the pressure of 5 bars. It is believed that carbon nano-particles can be coated on the friction surfaces and the interaction of nano-particles between surfaces can be improved the lubrication in the friction surfaces. Carbon nano-oilenhances the characteristics of the anti-wear and friction at the thrust slide-bearing of scroll compressors.

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An Experimental Study on the Internal Flow Characteristics of a Jet Pump for the Smart UAV Fuel System (스마트무인기 연료계통 제트펌프의 내부 유동 특성에 관한 실험적 연구)

  • Lee, Yoon-Kwon;Lee, Chang-Ho;Choi, Hee-Joo;Lee, Jee-Keun
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.32 no.2
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    • pp.107-116
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    • 2008
  • The jet pumps are widely used to transfer the fuel between the tanks in an aircraft fuel supply system. However detailed design procedures for determining the size of components of the jet pumps are not known so well. In this paper, the flow characteristics of the jet pump, which is applied in the fuel transfer system for the smart UAV (Unmanned Aerial Vehicle), were experimentally investigated using the acrylic jet pump model for the visualization of the internal flow. The pressure distributions within the jet pump were measured, and then the loss coefficients of each part were calculated. The effects of Reynolds number and the distances (S) between the exit of the primary nozzle and the mixing chamber entrance were investigated. In addition, cavitation phenomena were considered through the flow visualization inside the jet pump. As a conclusion from the experiment, the contraction shape of the primary nozzle has a strong effect on the loss coefficient of the nozzle and the cavitation occurrence. Cavitation starts around the nozzle exit, and then it propagates to the full flow fields of the jet pump.

Wind Tunnel Evaluation of Aerodynamic Coefficients of Thuja occidentalis and Mesh Net (풍동실험을 통한 방풍용 서양측백나무와 농업용방풍망의 공기역학계수 평가)

  • Lee, Sojin;Ha, Taehwan;Seo, Siyoung;Song, Hosung;Woo, Saemee;Jang, Yuna;Jung, Minwoong;Jo, Gwanggon;Han, Dukwoo;Hwang, Okhwa
    • Journal of The Korean Society of Agricultural Engineers
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    • v.63 no.5
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    • pp.63-71
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    • 2021
  • Windbreak forests, which have a windproof effect against strong winds, are known to be effective in reducing the spread of odors and dust emitted from livestock farms. The effect of reducing the spread of odors and dust can be estimated through numerical models such as computational fluid dynamics, which require aerodynamic coefficients of the windbreaks for accurate prediction of their performance. In this study, we aimed to evaluate the aerodynamic coefficients, Co, C1, C2, and α, of two windbreaks, Thuja occidentalis and a mesh net, through wind tunnel experiments. The aerodynamic coefficients were derived by the relation between the incoming wind speed and the pressure loss due to the windbreaks which was measured by differential pressure sensors. In order to estimate the change in the aerodynamic coefficient concerning various leaf density, the experiments were conducted repeatedly by removing the leaves gradually in various stages. The results showed that the power law regression model more suitable for coefficient evaluation compared to the Darcy-Forchheimer model.

Heat Transfer and Pressure Drop Characteristics of a Horizontal Channel Filled with Porous Media (다공성매질을 삽입한 수평채널의 열전달 및 압력강하 특성)

  • Son, Young-Seok;Shin, Jee-Young;Cho, Young-Il
    • Journal of Advanced Marine Engineering and Technology
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    • v.33 no.2
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    • pp.244-251
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    • 2009
  • Porous media have especially large surface area per volume, which contain complex fluid passage. If porous media can be applied to cool a CPU or an electronic device with large heat dissipation, it could result in heat transfer enhancement due to the enlargement of the heat transfer area and the flow disturbance. This study is aimed to identify the heat transfer and pressure drop characteristics of high-porosity metal foams in a horizontal channel. Experiment is performed with the various heat flux, velocity and pore density conditions. Permeabilities, which is deduced from Non-Darcy flow model, become lower with increasing pore density. Nusselt number also decreases with higher pore density. High pore density with same porosity case shows higher pressure loss due to the increase of surface area per unit volume. The fiction factor decreases rapidly with increase of Reynolds number in Darcy flow region. However, it converges to a constant value of the Ergun coefficient in Non-Darcy flow region.