• Title/Summary/Keyword: Class flow

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The Effect of Perceived Usefulness and Attitude of Adult Learners on Learning Flow and Learning Presence (성인학습자의 지각된 유용성과 태도가 학습몰입과 학습실재감에 미치는 영향)

  • Yu, Byeong Min;Park, Hye Jin;Jin, Hyun Seung
    • Journal of Agricultural Extension & Community Development
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    • v.23 no.4
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    • pp.449-457
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    • 2016
  • The purpose of this study are to examine the educational use of the Facebook and to examine the effects of the learners perceived usefulness, attitude and self-efficacy on learning flow and learning presence at university classes using social network service. The subjects of this study are 155 university students attending a class at a 4-year university in Seoul, and certain questions verified in the existing studies were modified, complemented, and used as a tool for measurement. The details of the purpose are as follows. First, it turned out that there were significant differences in learning flow and learning presence in accordance with the levels of the usefulness that learners perceived. It can be said that the higher the perceived level of usefulness, the higher the learning flow and learning presence. Second, it turned out that there were significant differences in learning flow and learning presence in accordance with the levels of learners' perceived attitudes. We can interpret such a result as suggesting that the higher a learner's perceived attitude, the higher the learning flow and learning presence.

The Effect of Self-leadership on Nursing Students' Learning Flow during the COVID-19 Pandemic: Mediating Effects of Psychosocial Well-being (COVID-19 팬데믹 상황에서 온라인 수업을 경험한 간호대학생의 셀프리더십이 학습몰입에 미치는 영향: 사회심리적 건강의 매개효과를 중심으로)

  • Park, Ju Young;Kang, Min Ju;Park, Chan Gyu;Bae, Taebin;Yu, Seo Hui;Ha, Jiyeon
    • Journal of the Korean Society of School Health
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    • v.35 no.2
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    • pp.41-48
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    • 2022
  • Purpose: The purpose of the study was to investigate the mediating effects of psychosocial well-being on the relationship between self-leadership and learning flow in nursing students. Methods: A total of 148 nursing students with online class experience participated in the study. The data were analyzed using the independent t-test, Pearson's correlation coefficient, PROCESS macro, and bootstrapping methods with SPSS Statistics 26.0. Results: The results showed that self-leadership, learning flow, and psychosocial well-being were significantly correlated, and self-leadership had a direct effect on learning flow. In other words, the higher the level of self-leadership, the higher the learning flow of nursing students. Psychosocial well-being was partially mediated by self-leadership and learning flow. Conclusion: It is necessary to develop and implement programs for self-leadership and psychosocial well-being enhancement as a strategy to enhance nursing students' learning flow.

An Optimization for Flow Control Butterfly Valve using Grey Relational Analysis (회색 관계 분석을 이용한 유량 제어용 버터플라이밸브 형상 최적화)

  • Lee, Sang Beom;Lee, Dong Myung
    • Journal of Korean Society of Coastal and Ocean Engineers
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    • v.26 no.6
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    • pp.359-366
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    • 2014
  • This paper considered optimization method of appending a shape on a disc in an attempt to improve core functions, which are inherent in flow characteristics. The paper also verifies the optimization method of appendage shape with a Class 150 200A Butterfly valve. Then the design of experiment (DOE) with an orthogonal array is performed to analyze the effect of form parameters by grey relational analysis and analysis of mean (ANOM). And this study sets flow coefficient as an object functions for optimization, and the conventional disc model and the optimal appendage shape on disc model are compared by computational fluid analysis. The paper concludes that an optimal appendage shape on disc model achieves wider usability by a wider operating range.

Design of Mixing Head Part of Combustion Chamber for 8tonf Class Staged Combustion Cycle Rocket Engine (8톤급 다단연소 사이클 로켓엔진 연소기 혼합헤드 설계)

  • Kim, Dongki;Ha, Seong up;Moon, Il yoon;Moon, Insang
    • Journal of Aerospace System Engineering
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    • v.9 no.2
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    • pp.34-40
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    • 2015
  • Staged combustion cycle engines are well known to have high combustion efficiencies and specific impulse. In this study, design of mixing head part of combustion chamber for 8tonf class staged combustion cycle rocket engine (ES-08) was performed. Structural stability of the mixing head part of the combustion chamber is very important design factor because it is loaded by high temperature and high pressure of fuel and oxidizer as well as by thrust load simultaneously. Uniformity of flow distributions of the propellants to the injectors is also important factor. First, a basic configuration for the ES-08 mixing head part was designed on the basis of the structural design requirements. And then, the structural analyses were performed on the basic configuration as well as some of reinforced configurations. As the structural analyses results, the most stable configuration was selected for the ES-08 mixing head part. In order to examine the uniformity of the flow distributions of the propellants through the manifold of the mixing head, flow analysis was performed based on the selected configuration. The results of the flow analysis showed that the fuel and the oxidizer were uniformly supplied to the injector.

Combustion Performance of a Full-scale Liquid Rocket Thrust Chamber Using Kerosene as Coolant (실물형 액체로켓엔진 연소기 케로신냉각 연소시험 성능결과)

  • Han, Yeoung-Min;Kim, Jong-Gyu;Moon, Il-Yoon;Seo, Seong-Hyeon;Choi, Hwan-Seok;Lee, Soo-Yong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.11a
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    • pp.163-168
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    • 2006
  • The combustion performance tests of a 30 tonf-class full-scale combustion chamber performed with kerosene as a coolant were described. The combustion chamber has chamber pressure of 53bara and propellant flow mass rate of 90kg/s. Since it was first firing test for 30tonf-class combustion chamber using kerosene cooling, kerosene coolant mass flow rate of 32kg/s which correspond to 120% of design mass flow rate were performed. Then, the firing test with kerosene mass flow rate of 25kg/s were successfully performed. The test results are described and the results showed that the kerosene cooling performance of this combustion chamber is sufficient and the firing test with regenerative cooling is feasible.

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An Analysis on Mathematic Classes using Flanders Category System (Flanders 언어상호작용 분석법을 적용한 수학 교과 수업 분석)

  • Lee, Yoon-Gyeong;Lee, Joong-Kweon
    • Journal of Fisheries and Marine Sciences Education
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    • v.26 no.4
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    • pp.902-914
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    • 2014
  • The purpose of this study is to provide useful information by analysis on mathematic classes for improve interactions between teacher and student using the Flanders Category System. For this, mathematic classes were observed by videotapes and recorded, 10 recorded videotapes were selected for analysis the property of linguistic interaction. The collected videotapes and records materials were transcribed by Advanced Flanders(AF) analysis program version 3.54. The detail investigated topics for studying are as follows. 1) What is the property of the Flanders 10 code analysis results? 2) What is the property of main and subsidiary linguistic flow of interaction? 3) What is the property of the Flanders index analysis results? The results of this study are as follow: 1) In Flanders 10 code analysis results, teacher's non-directive speaking is 12.76%, teacher's Indicative speaking is 50.28%, student's reactive speaking is 4.07%, student's voluntary speaking is 9.66%. 2) Among the 10 classes, 5 classes' main flow is 'ask convergent question ${\rightarrow}$ student's reactive speaking ${\rightarrow}$ lecture ${\rightarrow}$ ask convergent question', 2 classes' main flow is 'lecture ${\rightarrow}$ ask convergent question ${\rightarrow}$ student's reactive speaking ${\rightarrow}$ lecture', 3 classes' main and subsidiary flow is 'lecture ${\rightarrow}$ ask convergent question ${\rightarrow}$ lecture ${\rightarrow}$ work'. 3) In indices results, revised I/d ratio, student's speaking ratio, student question, wide answer ratio are higher than analysis standard and indirect ratio, teacher's question ratio are lower than analysis standard.

Effect of fineness of high lime fly ash on pozzolanic reactivity and ASR mitigation

  • Afshinnia, Kaveh;Rangaraju, Prasada R.
    • Computers and Concrete
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    • v.20 no.2
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    • pp.197-204
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    • 2017
  • Typically, high lime fly ash (Class C) has been characterized as a fly ash, which at lower replacement levels is not as effective as the low lime (Class F) fly ash, in mitigating alkali-silica reaction (ASR) in portland cement concrete. The influence of fineness of Class C, obtained by grinding virgin fly ash into finer particles, on its pozzolanic reactivity and ASR mitigation performance was investigated in this study. In order to assess the pozzolanic reactivity of mortar mixtures containing virgin or ground fly ashes, the strength activity index (SAI) test and thermo-gravimetric analysis (TGA) were conducted on the mortar cubes and paste samples, respectively, containing virgin fly ash or two ground fly ashes. In addition, to evaluate any improvement in the ASR mitigation of ground fly ashes compared to that of the virgin fly ash, the accelerated mortar bar test (AMBT) was conducted on the mortar mixtures containing different dosages of either virgin or ground fly ashes. In all tests crushed glass aggregate was used as a highly reactive aggregate. Results from this study showed that the finest fly ash (i.e., with an average particle size of 3.1 microns) could increase the flow ability along with the pozzolanic reactivity of the mortar mixture. However, results from this study suggested that the fineness of high lime fly ash does not seem to have any significant effect on ASR mitigation.

Low Pressure Firing Tests of 75-tonf-Class Channel Cooling Thrust Chamber (75톤급 채널냉각 연소기 저압연소시험)

  • Lim, Byoung-Jik;Han, Yeoung-Min;Kim, Jong-Gyu;Choi, Hwan-Seok
    • Journal of the Korean Society of Propulsion Engineers
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    • v.15 no.1
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    • pp.69-75
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    • 2011
  • Firing tests have been carried out for a technology demonstration model of 75-tonf-class combustor which is to be used on the liquid rocket engine of a Korean space launch vehicle. Firing tests were done at 50% of the nominal flow rate because of incapability of the test facility and limit of the test bed strength. Through the low pressure firing tests of 75-tonf-class channel cooling thrust chamber, operability and stability at the ignition and combustion phases were confirmed. Additionally it was foreseen that the 75-tonf-class thrust chamber would satisfy the performance requirements.

Low Pressure Firing Tests of 75-tonf-Class Channel Cooling Thrust Chamber (75톤급 채널냉각 연소기 저압연소시험)

  • Lim, Byoung-Jik;Han, Yeoung-Min;Kim, Jong-Gyu;Seo, Seong-Hyeon;Ahn, Kyu-Bok;Kim, Mun-Ki;Lee, Kwang-Jin;Choi, Hwan-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.05a
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    • pp.71-74
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    • 2010
  • Using the technology demonstration model of 75-tonf-class combustor which is expected to be used to the rocket engine of a korean space launch vehicle, 2 times of firing tests were carried out. Firing tests were done at 50% of the nominal flow rate because of incapability of the test facility and limit of the test bed strength. Through the low pressure firing tests of 75-tonf-class channel cooling thrust chamber, reliability and stability at the ignition and combustion phases were confirmed. Additionally it was foreseen that the 75-tonf-class thrust chamber would satisfy the performance requirements.

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Diesel Engine Intake Port Analysis Using Reverse-engineering Technique (리버스 엔지니어링을 통한 디젤엔진 흡기포트의 성능 비교)

  • Kim, Chang-Su;Park, Sung-Young
    • Transactions of the Korean Society of Automotive Engineers
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    • v.23 no.5
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    • pp.502-507
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    • 2015
  • In this paper, we built a three-dimensional model by applying reverse engineering techniques on targeting the intake port of 2900cc class diesel engine before that three-dimensional design technique is applied. The performance of the intake port is predicted and analysed using the computational flow analysis. Flow Coefficient and Swirl Ratio have been analyzed for two intake port models. One is the intake port for the diesel engine with plunger-type fuel system, and the other is for the diesel engine with CRDI fuel system. Computational result shows that the Flow Coefficient of the intake port with CRDI fuel system is increased upto 10 percentage compared with that with plunger-type. Also, the intake port with plunger-type has high Swirl Ratio at high valve lift, and the intake port with CRDI fuel system has high Swirl Ratio at relatively low valve lift. It is believed that because of high performance of the fuel injector, the intake port with CRDI fuel system is designed for more air amount and not much swirl flow at high valve lift. However, high swirl flow is required at low valve lift for initial fuel and air mixing. The result of this study may be useful for the re-manufacturing industry of automotive parts.