• 제목/요약/키워드: dynamic prediction method

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MPV 프레임의 피로수명 예측 (Fatigue Life Prediction of a Multi-Purpose Vehicle Frame)

  • 천인범;조규종
    • 한국자동차공학회논문집
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    • 제6권5호
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    • pp.146-152
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    • 1998
  • Recently, for the development of vehicle structures and components there is a tendency to increase using numerical simulation methods compared with practical tests for the estimation of the fatigue strength. In this study, an integrated powerful methodology is suggested for fatigue strength evaluation through development of the interface program to integrate dynamic analysis quasi-static stress analysis and fatigue analysis, which were so far used independently. To verify the presented evaluation method, a single and zigzag bump run test, 4-post road load simulation and driving durability test have been performed. The prediction results show a good agreement between analysis and test. This research indicates that the integrated life prediction methodology can be used as a reliable design tool in the pre-prototype and prototype development stage, to reduce the expense and time of design iteration.

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천음속 미사일의 동안정성에 대한 충격파 영향 (Effect of Shock Waves on Dynamic Stability of Transonic Missiles)

  • 박수형;권장혁;허기훈;변우식
    • 한국항공우주학회지
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    • 제30권2호
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    • pp.12-20
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    • 2002
  • 천음속 미사일에 대한 동안정 미계수 예측을 위해 비정상 Euler 방정식 해석을 수행하고, 동안정 미계수를 구하기 위한 적분방법을 제시하였다. 현재 방법의 정확도와 효율성을 검증하기 위해 Basic Finner에 대한 계산결과를 실험치와 비교하였다. 또한, Model Finner에서 받음각, 마하수, 회전율에 따른 동안정 미계수들의 변화를 고찰하였다. 해석 결과 천음속 영역에서 핀 사이에 발생한 충격파가미사일의 피치안정성을 증진시킴을 알 수 있었다. 계산의 결과는 비정상 Euler 해석이 충분한 정확도로 동안정 계수의 예측에 적용될 수 있음을 보여준다.

역문제에 의한 구조물의 실동하중 해석 (Analysis of Practical Dynamic Force of Structure with Inverse Problem)

  • 송준혁;노홍길;김홍건;유효선;강희용;양성모
    • 한국공작기계학회논문집
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    • 제13권2호
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    • pp.75-80
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    • 2004
  • Vehicle structures are composed of many substructure connected to one another by various types of mechanical joints. In vehicle engineering it is important to study these connected structures under various dynamic forces for the evaluations of fatigue life and stress concentration exactly. It is difficult to obtain the accurate load history of specified positions because of the errors such as modeling, measurement and etc. In the beginning of design exact load data are actually necessary for the fatigue strength and life analysis to minimize the cost and time of designing. In this paper, the procedure of practical dynamic force determination is developed by the combination of the principal stresses of F. E. Analysis and experiment. Least square pseudo inverse matrix is adopted to obtain in inverse matrix of analyzed stresses matrix. The error minimization method utilizes the inaccurate measured error and the shifting error that the whole data is stiffed over real data. The least square criterion is adopted to avoid these non. Finally, to verify the proposed procedure, a bus is analyzed. This measurement and prediction technology can be extended to the structural modification of any geometric shape in complex structure.

모드분해기법을 이용한 동적 변형률신호로부터 변위응답추정 (Estimation of Displacement Responses from the Measured Dynamic Strain Signals Using Mode Decomposition Technique)

  • 김성완;장성진;김남식
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2008년도 춘계학술대회 논문집
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    • pp.109-117
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    • 2008
  • In this study, a method predicting the displacement responseof structures from the measured dynamic strain signal is proposed by using a mode decomposition technique. Dynamic loadings including wind and seismic loadings could be exerted to the bridge. In order to examine the bridge stability against these dynamic loadings, the prediction of displacement response is very important to evaluate bridge stability. Because it may be not easy for the displacement response to be acquired directly on site, an indirect method to predict the displacement response is needed. Thus, as an alternative for predicting the displacement response indirectly, the conversion of the measured strain signal into the displacement response is suggested, while the measured strain signal can be obtained using fiber optic Bragg-grating (FBG) sensors. To overcome such a problem, a mode decomposition technique was used in this study. The measured strain signal is decomposed into each modal component by using the empirical mode decomposition(EMD) as one of mode decomposition techniques. Then, the decomposed strain signals on each modal component are transformed into the modal displacement components. And the corresponding mode shapes can be also estimated by using the proper orthogonal decomposition(POD) from the measured strain signal. Thus, total displacement response could be predicted from combining the modal displacement components.

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An Overview of Flutter Prediction in Tests Based on Stability Criteria in Discrete-Time Domain

  • Matsuzaki, Yuji
    • International Journal of Aeronautical and Space Sciences
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    • 제12권4호
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    • pp.305-317
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    • 2011
  • This paper presents an overview on flutter boundary prediction in tests which is principally based on a system stability measure, named Jury's stability criterion, defined in the discrete-time domain, accompanied with the use of autoregressive moving-average (AR-MA) representation of a sampled sequence of wing responses excited by continuous air turbulences. Stability parameters applicable to two-, three- and multi-mode systems, that is, the flutter margin for discrete-time systems derived from Jury's criterion are also described. Actual applications of these measures to flutter tests performed in subsonic, transonic and supersonic wind tunnels, not only stationary flutter tests but also a nonstationary one in which the dynamic pressure increased in a fixed rate, are presented. An extension of the concept of nonstationary process approach to an analysis of flutter prediction of a morphing wing for which the instability takes place during the process of structural morphing will also be mentioned. Another extension of analytical approach to a multi-mode aeroelastic system is presented, too. Comparisons between the prediction based on the digital techniques mentioned above and the traditional damping method are given. A future possible application of the system stability approach to flight test will be finally discussed.

순차적 예측오차 방법에 의한 구조물의 모우드 계수 추정 (Identification of Model Parameters by Sequential Prediction Error Method)

  • 윤정방;이창근
    • 전산구조공학
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    • 제3권4호
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    • pp.143-148
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    • 1990
  • 다자유도를 가진 구조계로 부터 얻어진 동적거동의 측정치를 이용하여 구조물의 모우드계수를 추정하는 시간영역방법에 대해 연구하였다. 이를 위해 운동방정식을 실험적 모우드식으로 변환한 다음 이를 다시 이산시간 영역의 식인 ARMAX식으로 나타내었다. 순차적 예측 오차 방법을 이용하여 ARMAX식의 계수들을 추정한 후, 이들로 부터 구조물의 모우드 계수들을 계산하였다. 지진하중을 받는 3층 빌딩 구조물의 실험치를 이용하여 얻은 모우드 계수들은 서로 다른 실험간에 좋은 일치를 보였으며, 또한 계산된 계수들을 이용하여 다시 구한 구조물 응답의 시간이력들은 실험치들과 좋은 일치를 보였다.

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Prediction of Liquation Crack Initiation at HAZ of Laser Weldment Based on Strain Analysis at Elevated Temperature

  • Yamamoto, Motomichi;Shinozaki, Kenji;Kitamura, Mitsuru;Shirai, Makoto
    • 대한용접접합학회:학술대회논문집
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    • 대한용접접합학회 2002년도 Proceedings of the International Welding/Joining Conference-Korea
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    • pp.244-249
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    • 2002
  • The purpose of this study is to develope the prediction method of liquation crack initiation in HAZ of laser weldment. Thermal two dimensional strain analyses were performed by FEM for bead-on-plate welding in order to obtain the plastic strain at elevated temperature in HAZ of the laser weldment. From these results, it became clear that the plastic strain at elevated temperature affected liquation crack initiation in HAZ, and it could be proposed that the critical strain, which controlled liquation crack initiation, existed. Moreover, an attempt was made to develop thermal and dynamic three dimensional strain analysis method for the laser weldment in order to obtain the plastic strain at elevated temperature in HAZ of the laser weldment in more detail and precisely.

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Short-Term Load Forecasting Based on Sequential Relevance Vector Machine

  • Jang, Youngchan
    • Industrial Engineering and Management Systems
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    • 제14권3호
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    • pp.318-324
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    • 2015
  • This paper proposes a dynamic short-term load forecasting method that utilizes a new sequential learning algorithm based on Relevance Vector Machine (RVM). The method performs general optimization of weights and hyperparameters using the current relevance vectors and newly arriving data. By doing so, the proposed algorithm is trained with the most recent data. Consequently, it extends the RVM algorithm to real-time and nonstationary learning processes. The results of application of the proposed algorithm to prediction of electrical loads indicate that its accuracy is comparable to that of existing nonparametric learning algorithms. Further, the proposed model reduces computational complexity.

재결정 및 결정립 성장거동을 기초한 조직예측 모델에 대한 변수 결정방법 (Determination of Material Parameters for Microstructure Prediction Model Based on Recystallization and Grain Growth Behaviors)

  • 염종택;김정한;홍재근;박노광
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 2009년도 춘계학술대회 논문집
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    • pp.270-273
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    • 2009
  • This work describes a method of determining material parameters included in recrystallization and grain growth models. Focus is on the recrystallization and grain growth models of Ni-Fe base superalloy, Alloy 718. High temperature compression tests at different strain, strain rate and temperature conditions were chosen to determine the material parameters of dynamic recrystallization model. The critical strain and dynamically recrystallized grain size and fraction at various process variables were quantitated with the microstructual analysis and strain-stress relationships of the compression tests. Besides, isothermal heat treatments were utilized to fit the material constants included in the grain growth model. Verification of the determined material parameters is carried out by comparing the measured data obtained from other compression tests.

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피스톤슬랩에 의한 엔진 진동현상의 분석과 예측 (Analysis and Prediction of Piston-Slap Induced Vibration)

  • 권기웅;김양한
    • 대한기계학회논문집
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    • 제17권12호
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    • pp.3045-3054
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    • 1993
  • The mechanics related with piston-slap induced vibration has been studied in terms of non-dimensionalized dynamic equation of motion, various non-dimensional parameters such as non-dimensional side-thrust force and non-dimensional impact velocity throughout the numerical simulation. Experimental verification on the suggested prediction method has been also performed by using single cylinder engine which was carefully designed and manufactured to wisely control the engine parameters, especially clearance and the mass of piston. The predicted and experimentally observed vibration signature confirm that the proposed method is practically useful.