• Title/Summary/Keyword: 시스템 모델링

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Mathematical Modeling and Simulation for Steady State of a 75-ton Liquid Propellant Rocket Engine (75톤급 액체로켓엔진 정상상태 과정의 수학적 모델링 및 시뮬레이션)

  • Lee, Kyelim;Cha, Jihyoung;Ko, Sangho;Park, Soon-Young;Jung, Eunhwan
    • Journal of Aerospace System Engineering
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    • v.11 no.5
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    • pp.6-12
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    • 2017
  • This paper deals with mathematical modeling of a 75-ton open-cycle Liquid Propellant Rocket Engine (LPRE) and the steady state simulation based on a nominal operating point. Each component of open-cycle LPRE may be classified into seven major categories using thermodynamics and dynamics characteristics. To simplify the simulation model of LPRE in this paper, we used four govern equations with assuming no heat transfer process. We confirmed the mathematical model of LPRE by using the error ratio and comparing the experiment data and simulation data in steady state, and checked the stability with the linearized model. Finally, we demonstrated the simulation model as compared to the transient response of experimental data.

A Study on the Design of Metal Chopsticks using 3D Modeling System -Focused on the utilization of Korean cultural elements- (3D 모델링 시스템을 활용한 금속젓가락 디자인 연구 -한국의 문화요소 활용을 중심으로-)

  • Yi, Kyu-Nam;Jo, Su-Im
    • Journal of Digital Convergence
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    • v.19 no.3
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    • pp.331-344
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    • 2021
  • The purposes of this study are to review the designs of chopsticks which are the tableware we use in our daily lives, and to explore the possibilities of 3D Modeling System applications to improve their designs that will add the beauty of dining by sublating uniform and limited designs of the Korean chopsticks. To do so, this researcher was produced prototypes to be a unique cultural content through delicate expression using 3D Modeling while utilizing the Korean cultural elements as the design elements. After its production, unique design for chopsticks could be developed with the Korean characteristics. Like the case of this prototype, 3D Modeling and 3D Printing can help seek the new designs of chopsticks and improve the quality by multiple simulations. Also, it will assist to develop cultural contents that can play a role of the Korean cultural goods.

Geometric Modeling of the Skin-Stringer Integrated Panel with Three-Dimensional Woven Composite (3차원 직조 복합재료 스킨-스트링거 일체형 패널의 기하학적 모델링)

  • Yeonhi, Kim;Hiyeop, Kim;Jungsun, Park;Joonhyung, Byun
    • Journal of Aerospace System Engineering
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    • v.16 no.6
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    • pp.8-17
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    • 2022
  • This paper presents a novel geometric modeling technique to predict the mechanical properties of an aircraft wing's skin-stringer integrated panel. Due to mechanical and adhesive fastening, this panel is vulnerable to stress concentration and debonding, so we designed it to integrate the skin and stringer using three-dimensional woven composites. Geometric modeling was conducted by measuring the geometric parameters of the specimen and defining the pattern of the yarns as functions. We used a weighted average model with iso-strain and iso-stress assumptions to predict the mechanical properties of the panel parts. We then compared the results of a finite element analysis with a compression test to verify the accuracy of our model. Our proposed technique proved to be more efficient than the traditional experimental method for predicting the mechanical properties of skin-stringer integrated panels.

Development of a Haptic Modeling and Editing (촉감 모델링 및 편집 툴 개발)

  • Seo, Yong-Won;Lee, Beom-Chan;Cha, Jong-Eun;Kim, Jong-Phil;Ryu, Je-Ha
    • 한국HCI학회:학술대회논문집
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    • 2007.02a
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    • pp.373-378
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    • 2007
  • 최근 들어 햅틱 분야는 디지털 콘텐츠를 만질 수 있게 촉감을 제공함으로써 의학, 교육, 군사, 엔터테인먼트, 방송 분야 등에서 널리 연구되고 있다. 그러나 햅틱 분야가 사용자에게 시청각 정보와 더불어 추가적인 촉감을 제공함으로써 보다 실감 있고 자연스러운 상호작용을 제공하는 등 여러 가지 장점을 가진 것에 비해 아직은 일반 사용자들에게 생소한 분야다. 그 이유 중 하나로 촉감 상호작용이 가능한 콘텐츠의 부재를 들 수 있다. 또한 최근에 가상환경(Virtual Environment, VR)에 관심이 증가 되고, 가상환경에 햅틱이라는 기술을 접목시키는 시도가 많이 일어나고 있어서, 촉감 모델링에 대한 욕구 또한 증대 되고 있다. 일반적으로 촉감 모델링은 Material properties를 가지고 있는 그래픽 모델들로 구성이 된다. 그래픽 모델링은 일반적인 모델링툴 (MAYA, 3D MAX, 기타 등)으로 할 수 있다. 하지만 촉감 관련된 촉감 모델들은 콘텐츠를 제작한 이후에 일일이 수작업으로 넣어 주어야 한다. 그래픽 모델링에서는 사용자가 직접 눈으로 확인 하면서 작업을 이루어 지기 때문에 직관적으로 이루어질 수 있다. 이와 비슷하게 촉감 모델링은 직관적인 모델링을 하기 위해서 사용자가 직접 촉감을 느껴 보면서 진행이 되어야 한다. 또한 그래픽 모델링과 촉감 모델링이 동시에 진행이 되지 않기 때문에 촉감 콘텐츠를 만드는데 시간이 많이 걸리게 되고 직관적이지 못하는 단점이 있다. 더 나아가서 이런 촉감 모델링을 포함한 모델링 높은 생산성을 위해서 신속히 이루어져야 한다. 이런 이유들 때문에 촉감 모델링을 위한 새로운 인터페이스가 필요하다. 본 논문에서는 촉감 상호작용이 가능한 촉감 콘텐츠를 직관적으로 생성하고 조작할 수 있게 하는 촉감 모델러를 기술한다. 촉감 모델러에서 사용자는 3 자유도 촉감 장치를 사용하여 3 차원의 콘텐츠 (정적 이거나 동적이거나 Deformation이 가능한 2D, 2.5D, 3D Scene)를 실시간으로 만져보면서 생성, 조작할 수 있는 촉감 사용자 인터페이스 (Haptic User Interface, HUI)를 통해서 콘텐츠의 표면 촉감 특성을 직관적으로 편집할 수 있다. 촉감 사용자인터페이스는 마우스로 조작하는 기존의 2 차원 그래픽 사용자 인터페이스를 포함하여 3 차원으로 사용자 인터페이스도 추가되어 있고 그 형태는 촉감 장치로 조작할 수 있는 버튼, 라디오버튼, 슬라이더, 조이스틱의 구성요소로 이루어져있다. 사용자는 각각의 구성요소를 조작하여 콘텐츠의 표면 촉감 특성 값을 바꾸고 촉감 사용자 인터페이스의 한 부분을 만져 그 촉감을 실시간으로 느껴봄으로써 직관적으로 특성 값을 정할 수 있다. 또한, XML 기반의 파일포맷을 제공함으로써 생성된 콘텐츠를 저장할 수 있고 저장된 콘텐츠를 불러오거나 다른 콘텐츠에 추가할 수 있다. 이러한 시스템은 햅틱이라는 분야를 잘 모르는 사람들도 직관적으로 촉감 모델링을 하는데 큰 도움을 줄 수 있을 것이다.

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Software-In-the-Loop based Power Management System Modeling & Simulation for a Liquefied Natural Gas Carrier (SIL 기반 액화천연가스운반선 전력관리시스템의 모델링 및 시뮬레이션)

  • Lee, Kwangkook
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.21 no.6
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    • pp.1218-1224
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    • 2017
  • With the increasing risk in building liquefied natural gas carriers (LNGC), pre-simulation of various scenarios is required for system integration and safe operation. In particular, the power management system (PMS) is an important part of the LNGC; it works in tight integration with the power control systems to achieve the desired performance and safety. To verify and improve unpredicted errors, we implemented a simulation model of power generation and consumption for testing PMS based on software-in-the-loop (SIL) method. To control and verify the PMS, numeric and physical simulation modeling was undertaken utilizing MATLAB/Simulink. In addition, the simulation model was verified with a load sharing test scenario for a sea trial. This simulation allows shipbuilders to participate in new value-added markets such as commissioning, installation, operation, and maintenance.

A Study on Installed Performance Analysis Modelling for a Helicopter Propulsion System Considering Intake Loss (흡입구 손실을 고려한 헬리콥터 추진시스템의 장착성능 해석 모델에 관한 연구)

  • Kong, Chang-Duk;Koo, Young-Ju;Kho, Seong-Hee;Ki, Ja-Young;Cha, Bong-Jun;Yu, Hyeok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.05a
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    • pp.263-267
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    • 2008
  • In this work the realistic install performance analysis of a helicopter was performed together with power extraction enabling to operate auxiliary system as well as intake pressure loss, loss due to bleed air, etc. which must be considered in practical propulsion system's performance modelling to be installed to the airframe. The pressure loss occurring in intake was estimated from the intake performance map with relationships of Mach Number and pressure loss. In order to evaluate the proposed installed performance model, the experimental data for comparison must be needed when mounted in propulsion system. However because of lack of accessibility to such real data at the moment, the alternative way was made through comparison that the analysis results by the proposed model were compared with a wellknown commercial program GASTURB's analysis results. The validity of the proposed installed performance model was consequently confirmed because its average deferences from the GASTURB's results were within 0.5%.

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A study of structure modeling of the stratum corneum on the hydration (보습상태에서 피부각질의 구조 모델링에 관한 연구)

  • Kim, Jeong-Lae;Kim, Hye-Ju
    • The Journal of the Convergence on Culture Technology
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    • v.3 no.3
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    • pp.31-36
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    • 2017
  • We are made up to the variation of the structure modeling of the stratum corneum by the skin on the hydration. The given skin structure is consist of the control level of the intercellular route and transcellular route, and is confirmed to the variation of the modeling for algorithm. Hydration condition is consisted to modeling by the size, form and combination, that skin impedance is appeared to result the value of measurement by the several layer such as forms of ${\xi}-R-SC-RH$, ${\xi}-R-SL-RH$, ${\xi}-R-SG-RH$, ${\xi}-R-SS-RH$ and ${\xi}-R-SB-RH$. Hydration condition is showed to the alteration difference value of S-Corneum, S-Lucidum, S-Granulosum, S-Spinosum and S-Basale. And, composition condition was constructed with the alteration modeling that was established to separate the division parts for conversion system. We will be possible to progress the improvement effectiveness of the skin and to consist of the continuous hydration control system for functional on the skin. We will be possible to progress the improvement effectiveness of the skin and to consist of the continuous penetration control system for functional energy on the skin.

Process Simulation and Optimization of Fuel Cell System including CFD Modeling of Diesel Desulfurizer Unit Process (디젤탈황 단위공정의 CFD 모델링을 포함한 연료전지 시스템 공정설계 및 최적화)

  • Choi, Chang Yong;Im, Do Jin
    • Korean Chemical Engineering Research
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    • v.56 no.3
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    • pp.421-429
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    • 2018
  • We performed process and CFD simulations of a 100 kW fuel cell system. By process simulation, we derived the input flow rate of each unit process and the recycle diesel flow rate. Through CFD simulation considering the recycle diesel flow, more efficient operational condition was found. Using 6 desulfurize reactors, a TSA process for a 100 kW fuel cell system was successfully constructed. Heat interference between reactors was found to be negligible. These results will contribute to increasing the efficiency of fuel cell system and the developed desulfurizing module design will contribute to the clean petrochemical technology as well as fuel cell systems.

KSR-III 비행시험 발사 시나리오 개발

  • Shin, Myoung-Ho;Seo, Jin-Ho;Kim, Kwang-Soo;Hong, Il-Hi
    • Aerospace Engineering and Technology
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    • v.2 no.1
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    • pp.140-152
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    • 2003
  • Scenario is a guiding principle of launch operation and control for rocket and ground support system. Therefore, developing a scenario is the first step to prepare for rocket launch, which is a critical task for success of KSR-III flight test. The launch scenario for KSR-III flight test is a procedural sequence of command and control signals to be given to rocket and ground support systems. In this paper, the UML object modeling method is applied to development of a launch scenario. First, the subsystems of the launch system are modeled by objects, and then the interfaces between each two subsystems are modeled by association links. The finally obtained object diagram of KSR-III launch system is used to analyzing flow of data and commands and control signals, and interactions. The scenario includes the sequences of pre-launch/launch operations and emergency operations.

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Nonlinear Modeling of Super-RENS System Using a Neural Networks (신경망을 이용한 Super-RENS 시스템의 비선형 모델링)

  • Seo, Man-Jung;Im, Sung-Bin;Lee, Jae-Jin
    • Journal of the Institute of Electronics Engineers of Korea TC
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    • v.45 no.3
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    • pp.53-60
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    • 2008
  • Recently, various recording technologies are studied for optical data storage. After standardization of BD (Blue-ray Disc) and HD-DVD (High-Definition Digital Versatile Disc), the industry is looking for a suitable technology for next generation optical data storage. Super-RENS (Super-resolution near field structure) technique, which is capable of compatibility with other systems, is one of next optical data storage. In this paper, we analyze the nonlinearity of Super-RENS read-out signal through the bicoherence test, which uses HOS (Higher-Order Statistics) and apply neural networks for nonlinear modeling. The model structure considered in this paper is the NARX (Nonlinear AutoRegressive eXogenous) model. The experiment results indicate that the read-out signals have nonlinear characteristics. In addition, it verified the possibility that neural networks can be utilized for nonlinear modeling of Super-RENS systems.