• Title/Summary/Keyword: low velocity

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Cu와 Cu-35Zn 합금의 저주기 피로에 대한 음향특성 평가

  • 김정석;권숙인;안봉영;이승석
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2004.05a
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    • pp.72-72
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    • 2004
  • 대부분의 금속 재료는 제조 공정 중에 인장, 압축, 압연, 압출, 인발 등 소성 변형을 수반하는 가공의 단계를 거치게 된다. 가공 단계에서 가해준 변형률 및 이에 따라 형성된 전위구조 등은 생산재의 기계적 성질에 많은 영향을 미친다. 그리고 소성 변형이 수반되는 또 하나의 과정은 피로, 크리프 손상 등의 소성 변형을 수반하게 되는 기계적 손상이다 이러한 기계적 손상에 의해서도 전위가 도입되며, 전위의 집적부위에서 균열이 생성되기도 한다. 따라서 기계적 손상을 비파괴적으로 평가하는데 있어서도 소성 변형의 영향을 파악하는 것이 하나의 중요한 문제가 된다.(중략)

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Muscle Fatigue Monitoring Using Adaptive Digital Filter (적응 디지철 필터를 이용한 근육 피로도의 측정)

  • 최영환;변윤식;김철주;김성환
    • Journal of the Korean Institute of Telematics and Electronics
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    • v.25 no.9
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    • pp.1074-1080
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    • 1988
  • A new approach to the measurement of muscle fatigue by adaptive digital filtering algorithm is proposed. Unlike previously reported methods, it can estimate the muscle fatigue at every sample as the EMG signal statistics change. As a result, the muscle conduction velocity ranged between 4.2-5m/s at low tension and 3-4m/s at fatigue state.

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On the Aeroelastic Characterisrics for the Flight Vehicle of Wing-Body Combination (익동체(翼胴體)의 공력탄성학적특성(空力彈性學的特性)에 관한 연구(硏究))

  • Hae-Kyong,Lee
    • Bulletin of the Society of Naval Architects of Korea
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    • v.10 no.1
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    • pp.27-32
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    • 1973
  • This paper shows the method for obtaining the body flutter velocity and frequency for flight body which consists of low aspect ratio wing and body combination by assuming slender body of cylinderical shell structure. The stiffness matrix of the cylinderical shell is represented from Donnel eq. by the finite difference method, and also unsteady aerodynamic influence matrix is represented by the Doublet Lattice Method of Albano & Rodden. The flutter matrix can be obtained from those matrices.

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Molecular dynamics simulation of ultra-low energy ion implantation for GSI device technology development (GSI소자 개발을 위한 극 저 에너지 이온 주입에 대한 분자 역학 시뮬레이션)

  • 강정원;손명식;황호정
    • Journal of the Korean Institute of Telematics and Electronics D
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    • v.35D no.3
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    • pp.18-27
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    • 1998
  • Molecular dynamicsinvestigations of ion implantation considering point defect generation were performed with ion energies in the range of ~1keV, Simulation starts perfect diamond cubic lattice site. Stillinger-Weber potential and ZBL potential were used to calculate forces between atoms. We have simulated slowing-down of ion velocity, ion trajectory and coupled-coing between ion and silicon. We also discussed distribution of point defect using rdial distribution function. We found that interstitial produced by ion bombardment mainly formed interstitial cluster.

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Analysis of Electron Transport Coefficients in Low Voltage Air Circuit Breaker Using MCS and BE (몬테칼로 시뮬레이션과 볼츠만 방정식을 이용한 저전압 기중차단기의 전자수송계수 특성파악)

  • 하성철;서상현
    • Journal of the Korean Institute of Electrical and Electronic Material Engineers
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    • v.16 no.2
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    • pp.168-172
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    • 2003
  • The electron transport coefficients in Air is analysed in range of E/Nvalues from 100~1000(Td) by a MCS and BE method. This paper have calculated W, ND$\sub$L/, ND$\sub$T/, Mean energy mixtures by N$_2$+O$_2$. The results gained that the values of the electron swarm parameters such as the electron drift velocity, longitudinal and transverse diffusion coefficients.

Wind Energy Charger Using Breaking and Power Conversation Switch (제동 및 전력변환 겸용 스위치를 이용한 풍력발전용 충전장치)

  • Ju, Hong-Ju;Lee, Hwa-Chun;Park, Sung-Jun
    • Proceedings of the KIPE Conference
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    • 2007.07a
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    • pp.80-82
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    • 2007
  • In this paper, we proposed new maximum electric power tracking algorithm by composing Buck-boost chopper circuit to charge electric power from wind energy generator which is under low and high wind velocity. The break function is also proposed with the existed buck-boost chopper switch. We made a proto-type as a lab level to verify appropriateness of using proposed circuit.

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Study on the compensation algorithm for inertial navigation system

  • Kim Hwan-Seong;NGUYEN DuyAnh
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
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    • 2005.10a
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    • pp.47-52
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    • 2005
  • This paper describes how a relatively compensate the error of position by using low cost Inertial Measurement Unit (IMU) has been evaluated and compared with the well established method based on a Kalman Filter(KF). The compensation algorithm by using IMU have been applied to the problem of integrating information from an Inertial Navigation System (INS). The KF is to estimate and compensate the errors of an INS by using the integrated INS velocity and position. We verify the proposed algorithm by simulation results.

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A POSTERIORI ERROR ESTIMATORS FOR THE STABILIZED LOW-ORDER FINITE ELEMENT DISCRETIZATION OF THE STOKES EQUATIONS BASED ON LOCAL PROBLEMS

  • KIM, KWANG-YEON
    • Journal of the Korean Society for Industrial and Applied Mathematics
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    • v.21 no.4
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    • pp.203-214
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    • 2017
  • In this paper we propose and analyze two a posteriori error estimators for the stabilized $P_1/P_1$ finite element discretization of the Stokes equations. These error estimators are computed by solving local Poisson or Stokes problems on elements of the underlying triangulation. We establish their asymptotic exactness with respect to the velocity error under certain conditions on the triangulation and the regularity of the exact solution.

Integrated Navigation System with Low-cost GPS and INS (저가형 GPS와 INS를 이용한 복합항법 시스템 개발)

  • Kim, Min-Ho;Song, Hyun-Min;Kim, Jeong-Rae
    • Journal of Aerospace System Engineering
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    • v.4 no.3
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    • pp.17-23
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    • 2010
  • GPS sensors provide accurate position and velocity of moving vehicles. However, GPS is weak at intermittent signal loss and large position error. Combination with INS improves the GPS position accuracy during the GPS signal loss. In this paper, a fusion filter using GPS and INS is developed and its perfomance is analyzed with RC car and RC airplane experiments.

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A Study on Shaft Fatigue Strength due to Torsional Vibrations in Two Stroke Low Speed Diesel Engines (저속 2행정 디젤엔진의 과도 비틀림 진동에 의한 축계 피로 강도에 관한 연구)

  • Lee, D.C.;Kim, S.H.
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2006.11a
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    • pp.786-791
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    • 2006
  • Two stroke low speed diesel engines are mainly used for marine propulsion or power plant prime mover. These have many merits such as higher thermal efficiency, mobility and durability. However various annoying vibrations sometimes occur in ships or at the plant itself. Of these vibrations, torsional vibration is very important and it should be carefully investigated during the initial design stage for engine's safe operation. In this paper authors suggest a new estimation method of for shaft's can be calculated equivalently from accumulated fatigue cycles number due to torsional vibration. The 6S70MC-C($25,320ps{\times}91rpm$) engine for ship propulsion was selected as a case study, and the accumulated fatigue cycles numbers for shafting life time converted from the measured angular velocity and torsional vibration stress was calculated. This new method can be realized and confirmed in test model ship with two stroke low speed diesel engine.

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