• Title/Summary/Keyword: 유동모드

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Dynamic Correction of DES Model Constant for the Advanced Prediction of Supersonic Base Flow (초음속 기저유동의 우수한 예측을 위한 DES 모델상수의 동적 보정)

  • Shin, Jae-Ryul;Choi, Jeong-Yeol
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.38 no.2
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    • pp.99-110
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    • 2010
  • The DES analysis of strong compressibility flow, LES mode is intentionally performed in boundary layer with the conventional empirical constant $C_{DES}$ value of 0.65. In this study, an expression is suggested to determine the $C_{DES}$ value dynamically by using a distribution function of the ratio of turbulence length scale and wall distance which is used in S-A DDES model for RANS mode protection. The application of the dynamic $C_{DES}$ presents better prediction than previous results those used constant but different $C_{DES}$ values.

램제트 엔진 흡입구의 점성 유동장 수치계산

  • 강호철;신동신
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2002.04a
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    • pp.59-59
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    • 2002
  • 램제트 추진기관은 압축과정을 별도의 부품 없이 형상에 의해서 감속하여 연소 압력비를 얻는다. 따라서 구동 마하수와 형상에 의해 흡입과정의 압축 효율이 결정된다. 설계점은 충분한 유량을 확보 할 수 있는 유량과 충격파 각을 조절하여 전압력 손실을 줄이도록 고려되어야 한다. 또한 연소가 일어나면 연소실 압력이 배압으로 작용하고 비행시에 받음각은 변하므로 이에 따른 성능 분석도 고려 되어야 할 사항이다. 본 연구는 국내에서 실험한 형상에 대해 수치계산을 수행하여 코드의 검증과 아울러 램제트 유동장의 수치적 시뮬레이션도 설계단계에서 하나의 도구로 이용할 수 있음을 보여준다. 실험에서는 배압 조건을 얻기 위해 유동 블록키지를 유로 내에 두어 상응하는 배압을 얻었지만 본 계산에서는 압력 경계조건을 직접 사용하였다. 유동이 비정상 특성을 가지므로 시간 정확도를 이차로 가지도록 이중시간 전진법을 사용하였다. 사용한 압력비는 충격파가 카울 끝에 닿는 임계상태에 가까운 12, 13, 14에 대해 계산을 수행하였고 부스터모드로 흡입구 끝이 막혀 있다가 램제트 모드로 바뀌어 연소실 압력이 위의 압력비라고 가정할 때의 비정상 천이 과정을 계산해 보았다. 본 계산은 흡입구 부분만을 떼어놓고 적절한 가정 하에 수행되었지만 연소실 내부도 비정상 특성을 가지므로 흡입구와 연소실을 동시에 같이 계산해야한다. 추후에 전체적인 계산을 진행하기 위한 전 단계로 흡입구 계산만을 수행하여 실험과 잘 일치하는 계산 결과를 얻었고 전체 계산을 위한 연구는 진행 중에 있다.

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Optimal Design of New Magnetorheological Mount for Diesel Engines of Ships (선박용 디젤엔진을 위한 새로운 MR 마운트의 최적설계)

  • Do, Xuan-Phu;Park, Joon-Hee;Woo, Jae-Kwan;Choi, Seung-Bok
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.23 no.3
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    • pp.209-217
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    • 2013
  • This paper presents an optimal design of a magnetorheological(MR) fluid-based mount(MR mount) that can be used for to vibration control in diesel engines of ships. In this work, a mount that uses mixed-modes(squeeze mode, flow mode, and shear mode) is proposed and designed. To determine the actuating damping force of the MR mount required for efficient vibration control, the excitation force from a diesel engine is analyzed. In this analysis, a model of a V-type engine is considered. The relationship between the velocity and pressure of gas in terms of the torque acting on the piston is derived. Subsequently, by integrating the field-dependent rheological properties of commercially available MR fluid with the excitation force, the appropriate size of the MR mount is designed. In addition, to achieve the maximum actuating force under geometric constraints, design optimization is undertaken using the ANSYS parametric design language software. Through magnetic density analysis, optimal design parameters such as the bottom gap and radius of coil are determined.

Optimal Design of New MR Mount for Diesel Engine of Ship (선박디젤엔진을 위한 새로운 MR 마운트의 최적설계)

  • Do, Xuan-Phu;Park, Joon-Hee;Woo, Jae-Kwan;Choi, Seung-Bok
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2012.10a
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    • pp.93-99
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    • 2012
  • This paper presents an optimal design of magnetorheological (MR) fluid based mount (MR mount in short) which can be applicable to vibration control of diesel engine of ship. In this work, a mixed - mode including squeeze mode, flow mode and shear mode is proposed and designed. In order to determine actuating damping force of MR mount required for efficient vibration control, excitation force from diesel engine is analyzed. In this analysis, a model of V-type engine is considered and the relationship between velocity and pressure of gas in torque of the piston is derived. Subsequently, by integrating the field-dependent rheological properties of commercially available MR fluid with the excitation force an appropriate size of MR mount is designed. In addition, in order to achieve maximum actuating force with geometric constraints design optimization is undertaken using ANSYS software. Through the magnetic density analysis, optimal design parameters such as bottom gap and radius of coil are determined.

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An Experimental Study on Mode ll Fracture Toughness Determination of Rock (암석의 전단 파괴인성 측정에 관한 실험적 연구)

  • 윤정석;전석원
    • Tunnel and Underground Space
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    • v.13 no.1
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    • pp.64-75
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    • 2003
  • This study presents a newly suggested test method of Mode II fracture toughness measurement called "Punch Through Shear Test" which was originally proposed by Backers and Stephansson in 2001. The purpose of this study is to check the validity of the suggested testing method by performing Mode II fracture toughness tests for Daejeon Granite. In addition, the optimal specimen geometry for the testing and the relation between Mode II fracture toughness and confining pressure were also investigated. Fractured surface was observed to be very smooth with lots of rock debris which came off fracture surface which obviously implies that the surface was sheared off. This confirms that Mode II fracturing actually occurred. In addition, numerical analyses including continuum analysis, particle flow code analysis and crack propagation simulations were performed. Results of these numerical analyses indicated that the cracks occurred in the specimen were predominantly in Mode II and these cracks led to failure of the test specimen. From this investigation, it can be concluded that the newly suggested "Punch Through Shear Test" method provides a reliable means of determining the Mode II fracture toughness. fracture toughness.

Numerical Analysis on Screech Tone in a Supersonic Jet (숯계산에 의한 초음속 제트의 스크리티 톤 소음 해석)

  • Kim, Yong-Seok;Lee, Duck-Joo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.2
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    • pp.94-100
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    • 2007
  • An axisymmetric supersonic jet screech in the Mach number range from 1.07 to 1.2 is numerically simulated. The axisymmetric mode is the dominant screech mode for an axisymmetric jet. The Reynolds-averaged Navier-Stokes equations in the conjunction with a modified Spalart-Allmaras turbulence model are employed. A high resolution finite volume essentially non-oscillatory(ENO) schemes are used along with nonreflecting characteristic boundary conditions that are crucial to screech tone computations to accurately capture the sound waves, shock-cell structures and large-scale instability waves.

Quantitative Visualization of Ventilation Flow for Defrost Mode in a Real Passenger Car (제상모드에 대한 실차 내부 환기유동의 정량적 가시화 연구)

  • Lee, Jin-Pyung;Lee, Sang-Joon
    • Journal of the Korean Society of Visualization
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    • v.8 no.2
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    • pp.40-44
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    • 2010
  • Thermal comfort inside a passenger car has been receiving large attention in automobile industries. Especially, the performance of windshield defroster is important in the design of a car to ensure passenger comport and safety. Thereby, better understanding on the ventilation flow along the vehicle windshield is essential to evaluate the performance of windshield defroster. However, most previous studies dealt with the defrost flow using CFD (computational fluid dynamics) calculations or scale-down model experiments. In this study, a real commercial automobile was used to investigate the flow discharged from the vehicle defroster and the ventilation flow along the windshield using a PIV velocity field measurement technique. The experimental data would be useful to understand the flow characteristics in detail and also can be used to validate numerical predictions.

Numerical Analysis and Control of Open Cavity Flow (열린 공동 유동의 수치적 모사 및 Jet Blowing 을 이용한 제어)

  • Chang, Kyung-Sik;Park, Seung-O;Choi, Hun-Ki
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.30 no.5
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    • pp.101-108
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    • 2002
  • A numerical simulation of an incompressible cavity flow is conducted. Two dimensional Navier-Stokes equations are integrated using staggered grid and a finite volume method with C-QUICK scheme for spatial derivatives and fully implicit scheme for the time derivatives. SIMPLE-C algorithm is employed to solve the pressure field. Computational results show that the third eddy is generated in the shear layer mode but not in the steady mode. This signifies that the third eddy plays an important role in cavity flow stability. As a means to control the flow, jet blowing is applied to a position below the cavity upstream edge. Effects of flow control parameters on the stability such as the frequency, the phase, and the velocity magnitude are reported.

Design of Positioning System Using Beacon Mode of Bluetooth Module (블루투스 모듈의 비콘 모드를 이용한 위치 탐지 시스템 설계)

  • You, Dong-ju;Jang, Si-Woong
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • 2019.05a
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    • pp.122-124
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    • 2019
  • 최근 IoT 시스템의 관심도가 높아지고 있어 기본 활용 기술의 방법 중 블루투스 비콘 모드를 이용한 정확한 위치 탐지 방법에 대한 연구가 진행되고 있다. 본 논문에서는 블루투스 모듈의 비콘 모드를 활성화하여 불특정 다수의 사용자들에게서 획득한 정보의 고유아이디(UUID, Universally Unique Identifiers) 식별 및 특정 기기의 위치를 파악하여 해당 UUID의 위치 탐지 방법을 제안하였다. 비콘 정보의 수신신호세기(RSSI, Received Signal Strength Indicator)값을 이용하여 불특정 사용자의 위치를 탐지하고, 설정된 RSSI의 범위 구간에 따라 탐지 객체의 IoT 모듈에 접근 여부를 판단하고, 접근이 감지되었을 때 해당 모듈의 IoT 모듈의 기능을 작동시키는 방식으로 활용할 수 있다. 또한, 위치 탐지의 정확성을 위해 RSSI의 데이터를 저장하고, 저장된 데이터 관찰을 통하여 해당 블루투스의 위치 데이터를 보다 정확하게 파악하는 시스템을 설계하였다.

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