• Title/Summary/Keyword: Flow configuration

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Effect of Primary Nozzle Configuration on the Flow and Transfer Characteristics in an Ejector System for Pellet Transfer (펠릿 이송용 이젝터의 구동노즐 구성에 따른 유동 및 이송특성에 관한 실험적 연구)

  • Kim, Keum-Kyu;Kim, Eui-Soo;Kang, Shin-Myoung;Lee, Jee-Keun;Rho, Byung-Joon
    • Transactions of the Korean Society of Automotive Engineers
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    • v.16 no.5
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    • pp.49-59
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    • 2008
  • The effects of design parameters on the pellet transport rate in the ejector system which is widely used in the production processes of automotive parts were investigated experimentally. The primary nozzle geometry, the area ratio (R) of nozzle exit cross-sectional area to mixing chamber cross-sectional area and the distance (S) from primary nozzle exit to mixing chamber entrance were considered as the design parameters. The area ratios of the primary nozzle were varied from R=0.10 to R=0.25, 0.30, 0.40 and 0.55. The primary nozzle was positioned at the non-dimensional distance (S/D) of 1.30, 1.87, 2.44, 3.00 and 3.75, normalized using the mixing chamber diameter (D). The design parameters were determined to run with high efficiency by measuring the pellets transport rate. The geometry and the area ratio (R) of the primary nozzle had an effect on the pellet transport rate of the ejector system, and the area ratio of R=0.3 was carefully selected after taking the minimum fluidization velocity and transport rate of applied pellets into account. The higher pellet transport rate with the variation of the distance (S/D) was observed at S/D of 2.44.

Aerodynamic Design of a Canard Controlled 2D Course Correction Fuze for Smart Munition (카나드 기반의 지능탄 조종 장치 공력설계)

  • Park, Ji-Hwan;Bae, Ju-Hyeon;Song, Min-Sup;Myong, Rho-Shin;Cho, Tae-Hwan
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.43 no.3
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    • pp.187-194
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    • 2015
  • Course correction munition is a smart projectile which improves its accuracy by the control mechanism equipped in the fuze section with canard. In this paper, various aerodynamic configurations of the fuze section were analysed by utilizing a semi-empirical method and a CFD method. A final canard configuration showing the least drag was then determined. During the CFD simulation, it was found that the k-${\omega}$ SST turbulence model combined with O-type grid base is suitable for the prediction of the base drag. Finally, the aerodynamic characteristics of the smart munition and the change of drag due to the canard installation were analysed.

Actual Feeling Service Model for Video-Media Contents (영상미디어콘텐츠에 대한 실감 서비스 모델)

  • Lee, Ji-Hye;Yoon, Yong-Ik
    • Journal of Digital Contents Society
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    • v.10 no.3
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    • pp.453-459
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    • 2009
  • In recently, as the interest of media contents increase among internet users, a variety of media contents are circulated in the web. Especially, video-media content in media contents attracts internet user's interest. In conjunction with web 2.0, internet users open and share their making contents by themselves. Their attitude about accepting media contents is not passive but aggressive. Additionally, they create new form of distribution of the flow. Video media content for distribution on the Web is created by experts to a professional content, but Web 2.0 era, the UCC (User Create Contents) in the form of self-produced content is the most. The generated media by the general internet users, but self-produced content, provides video information only and has limitations. To satisfy internet users as consumers in the web 2.0 eras, it has needed to provide actual feeling contents that add various effects not just simple media. Therefore, this paper represents the existing media content with simple information based on the concept of ontology and the meaning to the subject for the media content. We will provide an actual feeling how to offer the configuration of a service model (AF-VS : Actual Feeling Video Service).

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Model-based and wavelet-based fault detection and diagnosis for biomedical and manufacturing applications: Leading Towards Better Quality of Life

  • Kao, Imin;Li, Xiaolin;Tsai, Chia-Hung Dylan
    • Smart Structures and Systems
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    • v.5 no.2
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    • pp.153-171
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    • 2009
  • In this paper, the analytical fault detection and diagnosis (FDD) is presented using model-based and signal-based methodology with wavelet analysis on signals obtained from sensors and sensor networks. In the model-based FDD, we present the modeling of contact interface found in soft materials, including the biomedical contacts. Fingerprint analysis and signal-based FDD are also presented with an experimental framework consisting of a mechanical pneumatic system typically found in manufacturing automation. This diagnosis system focuses on the signal-based approach which employs multi-resolution wavelet decomposition of various sensor signals such as pressure, flow rate, etc., to determine leak configuration. Pattern recognition technique and analytical vectorized maps are developed to diagnose an unknown leakage based on the established FDD information using the affine mapping. Experimental studies and analysis are presented to illustrate the FDD methodology. Both model-based and wavelet-based FDD applied in contact interface and manufacturing automation have implication towards better quality of life by applying theory and practice to understand how effective diagnosis can be made using intelligent FDD. As an illustration, a model-based contact surface technology an benefit the diabetes with the detection of abnormal contact patterns that may result in ulceration if not detected and treated in time, thus, improving the quality of life of the patients. Ultimately, effective diagnosis using FDD with wavelet analysis, whether it is employed in biomedical applications or manufacturing automation, can have impacts on improving our quality of life.

Design and Performance Evaluation of Superstructure Modification for Air Drag Reduction of a Container Ship (공기저항 저감을 위한 컨테이너선 상부구조물 형상설계 및 성능평가)

  • Kim, Yoonsik;Kim, Kwang-Soo;Jeong, Seong-Wook;Jeong, Seung-Gyu;Van, Suak-Ho;Kim, Jin
    • Journal of the Society of Naval Architects of Korea
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    • v.52 no.1
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    • pp.8-18
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    • 2015
  • Reduction of the fuel oil consumption and corresponding greenhouse gas exhausted from ships is an important issue for today's ship design and shipping. Several concepts and devices on the superstructure of a container ship were suggested and tested in the wind tunnel to estimate the air drag reduction. As a preliminary performance evaluation, air drag contributions of each part of the superstructure and containers were estimated based on RANS simulation respectively. Air drag reduction efficiency of shape modification and add-on devices on the superstructure and containers was also estimated. Gap-protectors between containers and a visor in front of upper deck were found to be most effective for drag reduction. Wind tunnel tests had been carried out to confirm the drag reduction performance between the baseline(without any modification) configuration and two modified superstructure configurations which were designed and chosen based on the computation results. The test results with the modified configurations show considerable aerodynamic drag reduction, especially the gap-protectors between containers show the largest reduction for the wide range of heading angles. RANS computations for three configurations were performed and compared with the wind tunnel tests. Computation result shows the similar drag reduction trend with experiment for small heading angles. However, the computation result becomes less accurate as heading angle is increasing where the massively separated flow is spread over the leeward side.

Optimal Design and Combustion Analysis of Fuel-rich Gas Generator for Liquid Rocket Engine Based on RP-1 fuel (RP-1연료를 사용한 농후연소 가스발생기의 최적설계 및 연소해석)

  • 권순탁;이창진
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2003.05a
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    • pp.258-261
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    • 2003
  • The optimal design and combustion analysis of the gas generator for Liquid Rocket Engine (LRE) were performed. A fuel-rich gas generator in open cycle turbopump system was designed for 101on1 in thrust with RP-1/LOx combination. The optimal design was done for maximizing specific impulse of main combustion chamber with constraints of combustion temperature and power matching in turbopump system. Results of optimal design show the dimension of length, diameter, and contraction ratio of gas generator. The configuration of the gas generator and the condition for performance which can maximize the objective function were determined and found to meet the design constraints. Also, the combustion analysis was conducted to evaluate the performance of designed chamber and injector of gas generator. And the effect of the turbulence ring was investigated on the mixing enhancement in the chamber.

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The Study on Humoristic Beauty in Coptic Textiles Motifs (콥트 텍스타일에 나타난 유희적 골계미(滑稽美) 연구)

  • Jeong, Hye-Yeon;Lim, Choung-Soo
    • Journal of the Korea Fashion and Costume Design Association
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    • v.14 no.4
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    • pp.29-42
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    • 2012
  • Historically, the pattern and technology of Copts' textiles, who were a minority in Egypt, have been studied a lot in the textile sector due to its unique characteristics. Unlike ones in other regions that appeared around the same time, the overall configuration ratio of the patterns looks exaggerated or distorted because they expressed it plainly by interpreting the world with ordinary people's eyes. Also, because it had used mixed linen and woolen yarns, harsh expression way and the use of various colors have been one of the features in Coptic textiles. Coptic textiles, which have been developed along with the historical development of continued domination from neighboring countries, have expressed the effects of the Roman Empire, Christ, Christianity, and Islam on the pattern of its fabric. This study analyzed its characteristics which make people smile by the way of expressing a simple and humorous representation of the textiles and categorized them as Humoristic Beauty - the aesthetic category of humorous feature. In this study, the Humoristic Beauty in Coptic textiles has been analyzed in terms of the following three smiles; the smiles coincidental with the flow of time, the smiles made by the shaping of distorted proportions and appearance, and the smiles like folk-paintings made by a rustic expression way. This study shows the possibility of the further studies on the textile patterns history from a different angle. I look forward to more detailed analysis in the follow-up studies in the future.

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Performance Characteristics of Type II LiBr-H2O Absorption Heat Pump in Accordance with the Refrigerant Heat Exchanger Configuration (냉매 열교환기 구성방법에 따른 제 2종 흡수식 히트펌프의 성능 특성 변화에 관한 연구)

  • Lee, Chang Hyun;Yoon, Jun Seong;Kim, In Gwan;Kwon, Oh Kyung;Cha, Dong An;Bae, Kyung Jin;Kim, Min Su;Park, Chan Woo
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.29 no.7
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    • pp.373-384
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    • 2017
  • The objective of this study was to determine the effect of refrigerant heat exchanger on the performance of type II absorption heat pump performance using numerical analysis. Two heat exchange installation methods were used: solution to refrigerant and waste hot water to refrigerant. These methods were compared to the standard model of hot water flow without using refrigerant heat exchanger. When waste hot waters were bypassed to refrigerant heat exchanger, COP was not affected. However, steam mass generation rates were increased compared to those of the standard model. When solutions were bypassed to the refrigerant heat exchanger, results were different depending on the place where the solution rejoined. COP and steam mass generation rates were lower compared to those when waste heat water was passed to refrigerant heat exchanger. Thus, it is possible to obtain higher steam mass generation rates by using waste water and installing refrigerant heat exchanger.

A Study on Shock-induced Detonation in Gap Test (충격 전달에 의한 Gap Test의 폭굉 반응 해석)

  • Kim, Bohoon;Kang, Wonkyu;Jang, Seung-gyo;Park, Jungsu;Yoh, Jai-ick
    • Journal of the Korean Society of Propulsion Engineers
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    • v.20 no.2
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    • pp.75-85
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    • 2016
  • A pyrotechnic system consisting of donor/acceptor pair separated by a gap relies on shock attenuation characteristics of the gap material and shock sensitivity of the donor and acceptor charges. Despite of its common use, numerical study of such pyrotechnic train configuration is seldom reported because proper modeling of the full process requires precise capturing of the shock wave attenuation in the gap prior to triggering a full detonation of high explosive and accurate description of the high strain rate dynamics of the explosively loaded inert confinements. We apply a Eulerian level-set based multimaterial hydrocode with reactive flow models for pentolite donor and heavily aluminized RDX as acceptor charge. The complex shock interaction, critical gap thickness, acoustic impedance, and go/no-go characteristics of the gap test are quantitatively investigated.

액체로켓용 터빈시스템 설계

  • Choi, Chang-Ho;Kim, Jin-Han;Yang, Soo-Seok;Lee, Dae-Sung
    • Aerospace Engineering and Technology
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    • v.1 no.1
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    • pp.163-172
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    • 2002
  • The turbine system composed of a nozzle and a rotor is used to drive turbopumps while gas passes through the nozzle, potential energy is converted to kinematic energy, which forces the rotor blades to spin. In this study, an aerodynamic design of a turbine system is investigated using compressible fluid dynamic theories with some pre-determined design requirements (i.e.,pressure ratio, rotational speed, required power etc.) obtained from a liquid rocket engine (L.R.E.) system design. For simplicity of a turbine system, impulse-type rotor blades for open type L.R.E. have been chosen. Usually, the open-type turbine system requires low mass flow rate compared to the close-type system. In this study, a partial admission nozzle is adopted to maximize the efficiency of the close-type turbine system. A design methodology of the a turbine system has been introduced. Especially, a partial admission nozzle has been designed by means of simple empirical correlations between efficiency and configuration of the nozzle. Finally, a turbine system design for a 10 ton thrust level of L.R.E is presented.

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