• Title/Summary/Keyword: AIR 모델

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Analysis of the Effects of CO Poisoning and Air Bleeding on the Performance of a PEM Fuel Cell Stack using First-Order System Model (일차계 모델을 이용한 고분자전해질 연료전지 스택의 CO Poisoning 및 Air Bleeding 효과 분석)

  • Han, In-Su;Shin, Hyun Khil
    • Korean Chemical Engineering Research
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    • v.51 no.3
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    • pp.370-375
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    • 2013
  • We analyze the effects of CO poisoning and air bleeding on the performance of a PEM (polymer electrolyte membrane) fuel cell stack fabricated using commercial MEA (membrane electrode assembly). Dynamic response data from the experiments on the performance of a stack are identified by obtaining steady-state gains and time-constants of the first-order system model expressed as a first-order differential equation. It is found that the cell voltage of the stack decreases by 1.3-1.6 mV as the CO concentration rises by 1 ppm. The time elapsed to reach a new steady state after a change in the CO concentration is shortened as the magnitude of the change in the CO concentration increases. In general, the steady-state gain becomes bigger and the time-constant gets smaller with increasing the air concentration (air-bleeding level) in the reformate gas to restore the cell voltage. However, it is possible to recover 87%-96% of the original cell voltages, which are measured with free of CO, within 1-30 min by introducing the bleed air as much as 1% of the reformate gas into the stack.

The Future of Aerospace Weapon Systems based on Aerospace Technology Modeling (항공우주력 기술 모델링에 기반한 미래 항공우주 무기체계 발전방향)

  • Cho, Taehwan;Choi, Insoo;Lee, Soungsub
    • Journal of Advanced Navigation Technology
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    • v.24 no.5
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    • pp.368-373
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    • 2020
  • In order to systematically apply major technologies of the 4th Industrial Revolution to aerospace power development, an aerospace technology model is needed. The Propeller Model, which is an existing aerospace model, is a concept that operates a combination of altitude, speed, and distance, which are basic characteristics of aerospace. However, in the era of the 4th Industrial Revolution, a new model is needed because numerous technologies are used in convergence. In this paper, a jet engine model is proposed as a new aerospace technology model. Also, we propose a procedure for creating future aerospace weapon systems based on aerospace technology modeling, not on operational capability. The utilization of future battlefields and the study of the concept of advanced weapon systems in developed countries can create a new concept of weapon systems.

Uncertainty Analysis of a Pharmacokinetic Modeling for Inhalation Exposure of Benzene from the Use of Groundwater at Dwelling (거주지의 지하수사용에서 유래한 벤젠의 흡입노출에 대한 동적약리학 모델의 불확실성 분석)

  • 김상준;이현호;박지연;이유진;유동한;양지원
    • Journal of Soil and Groundwater Environment
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    • v.9 no.1
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    • pp.28-38
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    • 2004
  • This study presents the result of uncertainty and sensitivity analysis of a pharmacokinetic model which describes the distribution and removal of benzene at each organ when an indivisual inhales indoor contaminated air with benzene originated from groundwater. The pharmacokinetic model simulates the distribution of benzene deposited in organs of human body through inhalation of contaminated indoor air as well as degradation-metabolism in liver. This study focused on the uncertainty problem induced from the use of the single values for blood flow, partition coefficient, degradation constant, volume, etc. of each organ which was due to a lack of knowledge about these parameters or their measurements. To solve this problem, uncertainty analysis on the pharmacokinetic model was conducted simultaneously which would help understanding the risk assessment associated with VOCs.

A Study on the Interoperability of ROK Air Force Virtual and Constructive Simulation (공군 전투기 시뮬레이터와 워게임 모델의 V-C 연동에 대한 연구)

  • Kim, Yong Hwan;Song, Yong Seung;Kim, Chang Ouk
    • Journal of the Korea Society for Simulation
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    • v.28 no.2
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    • pp.169-177
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    • 2019
  • LVC(Live-Virtual-Constructive) training system is drawing attention due to changes in battlefield situation and the development of advanced information and communication technologies. The ROKAF(Republic of Korea Air Force) plans to construct LVC training system capable of scientific training. This paper analyzes the results of V-C interoperability test with three fighter simulators as virtual systems and a theater-level wargame model as a constructive system. The F-15K, KF-16, and FA-50 fighter simulators, which have different interoperable methods, were converted into a standard for simulation interoperability. Using the integrated field environment simulator, the fighter simulators established a mutually interoperable environment. In addition, the Changgong model, which is the representative training model of the Air Force, was converted to the standard for simulation interoperability, and the integrated model was implemented with optimized interoperability performance. Throughput experiments, It was confirmed that the fighter simulators and the war game model of the ROKAF could be interoperable with each other. The results of this study are expected to be a good reference for the future study of the ROKAF LVC training system.

Comparison and Validation Study on Computational Fluid Dynamics and Wind Tunnel Test Results of Standard Dynamics Model (표준 동안정 모델의 전산유체해석 및 풍동시험 결과 비교검증)

  • Cho, Donghyurn;Kim, Seung Pil;An, Eunhye;Choi, Younseok;Roh, Jisoo;Chung, Hyoung Seog
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.45 no.3
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    • pp.217-225
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    • 2017
  • This research represents comparison and validation of static aerodynamic results in different wind tunnel organizations and EFD-CFD results. KAFA conducted wind tunnel tests with Standard Dynamics Model(SDM) which is based on the NRC model, the same configuration of KARI; and then compared and analyzed similarities and differences of the data from KARI and NRC results for verifying the accuracy of wind tunnel tests. Also, We compared the result of CFD with that of wind tunnel tests and examined strakes effect in static characteristics which are attached on the forward fuselage of SDM for investigating the cause of some discrepancies. From this analysis, there are some discrepancies in Cm tendency between EFD-CFD and it did not show the big difference of aerodynamic characteristics by strake effects. Thus, we need to research additionally for analyzing the different cause of some discrepancies such as vortex structures by the rear strut or intake of SDM and regenerating grid resolution of CFD.

A Study of Machine Learning Model for Prediction of Swelling Waves Occurrence on East Sea (동해안 너울성 파도 예측을 위한 머신러닝 모델 연구)

  • Kang, Donghoon;Oh, Sejong
    • The Journal of Korean Institute of Information Technology
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    • v.17 no.9
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    • pp.11-17
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    • 2019
  • In recent years, damage and loss of life and property have been occurred frequently due to swelling waves in the East Sea. Swelling waves are not easy to predict because they are caused by various factors. In this research, we build a model for predicting the swelling waves occurrence in the East Coast of Korea using machine learning technique. We collect historical data of unloading interruption in the Pohang Port, and collect air pressure, wind speed, direction, water temperature data of the offshore Pohang Port. We select important variables for prediction, and test various machine learning prediction algorithms. As a result, tide level, water temperature, and air pressure were selected, and Random Forest model produced best performance. We confirm that Random Forest model shows best performance and it produces 88.86% of accuracy

The research on CFD turbulance models for comparison according to my secondary air injection into the combustion (연소로 내 2차 공기 분사에 따른 CFD 난류 모델 비교에 관한 연구)

  • Choi, Junhyuk;Choi, Chong-gun;Hwang, Seung-Sik;Shin, Donghoon;Chung, Tae-Yong
    • 한국연소학회:학술대회논문집
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    • 2012.11a
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    • pp.345-347
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    • 2012
  • The secondary air injection influences the flow of the combustion gas in the furnace. Therefore, the analysis of the furnace should be careful in the selection of the turbulent model with CFD. In this study, CFD results of several turbulent models were compared with experimental results. Analysis results suggest to select turbulent models in the furnace secondary air nozzle.

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Modification of Miller-Holzworth model for Korea (국내 적용을 위한 Miller-Holzworth 모델의 수정)

  • 장영기
    • Journal of Korean Society for Atmospheric Environment
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    • v.11 no.3
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    • pp.299-302
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    • 1995
  • Many air quality models have been used for Environmental impact assessments. Miller-Holzworth model suggested by Holzworth is a simple air quality model is frequently used for air quality assessments in korea. Miller-Holzworth model suggested by Holzworth is a simple air quality model for the ground-level area source, The model estimates the pollutants concentration averaged over the wind centerline. An error involved in the Miller-Holzworth model was first indentified by Calder in 1977. But the model has been used without correction for unsuitable cases in Korea. This paper corrected that error and modified model formulation for application to urban and rural areas.

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Numerical Analysis of Responses of a Elasto-plastic Tube under Kerosene-air Mixture Detonation (케로신-공기 혼합물의 비정상연소 모델과 탄소성 관의 동적 거동 수치해석)

  • Lee, Younghun;Gwak, Min-cheol;Yoh, Jai-ick
    • 한국연소학회:학술대회논문집
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    • 2015.12a
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    • pp.169-172
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    • 2015
  • This paper presents a numerical investigation on kerosene-air mixture detonation and behaviors of thermal elasto-plstic thin metal tube under detonation loading based on multi-material analysis. The detonation loading is modeled by the kerosene-air mixture detonation which is compared with CJ condition and experimental cell size. And the thermal softening effect on elasto-plstic model of metal tube is indicated by different dynamic response of detonation loaded tube in various temperature and tube thickness.

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Safety Analysis and Design Model for a Complex System like ATM(Air Traffic Management) System (ATM(Air Traffic Management) 시스템과 같은 복잡 시스템의 안전 분석 및 설계 모델)

  • Park, Joong-Yong
    • Journal of the Korean Society of Systems Engineering
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    • v.3 no.1
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    • pp.27-31
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    • 2007
  • A complex system like ATM(Air Traffic Management) has safety problem emerging from complex interactions between systems. In complex systems, malfunctions of components are not the only causes of critical accidents. To resolve this problem many researchers have proposed new safety analysis models for complex systems. This research is a way of improving safety analysis model focusing on systems engineering design model for ATM.

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