• 제목/요약/키워드: Asymmetric system

검색결과 702건 처리시간 0.028초

4MV 선형가속기에서의 비대칭 콜리메이터의 선량측정 (Dosimetric Measurement for 4MV X-Ray Linear Accelerator with Asymmetric Collimator System)

  • 이병용;최은경;장혜숙
    • 한국의학물리학회지:의학물리
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    • 제1권1호
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    • pp.69-73
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    • 1990
  • Dosimetric measurement of an asymmetric collimator system was performed, using water phantom system for 4MV X-ray linear accelerator. We have studied the system of dose calculation with those measured result. We compared the field size factor and the percent depth dose for asymmetric collimator to those factor for symmetric fields. The results show that we can use symmetric field data directly within 1% error, if we consider the off axis ratio(OAR).

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다단 비축대칭 부품의 단조 공정설계를 위한 단조품설계 자동화 (Development of Automated forging Design System for Forging Process Design of Stepped Asymmetric Parts)

  • 조해용;허종행;민규식
    • 한국정밀공학회지
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    • 제17권3호
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    • pp.102-107
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    • 2000
  • This study describes computer-aided design system for stepped asymmetric forgings. To establish the appropriate process sequence, an integrated approach based on a rule-base system was accomplished. This system has four modules, which are undercut prevention module, shape cognition module, 3D modelling module and corner/fillet correction module. These modules can be used independently or at all. The proposed shape cognition method could be widely used in forging design of asymmetric parts.

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Definition and calculation method of modal effective mass of asymmetric fluid-structure interaction system for seismic analysis

  • Yong-Hwa Heo;Jong-Oh Sun;Gyeong Ho Kim;Yeonseok Choo
    • Nuclear Engineering and Technology
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    • 제55권12호
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    • pp.4307-4316
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    • 2023
  • In this paper, modal effective mass for asymmetric fluid-structure interaction system is defined and equations for its calculation is derived. To establish consistency, modal effective mass in symmetric structure only system is briefly reviewed, followed by a definition of the modal effective mass in asymmetric system. The equations for calculating modal effective mass in asymmetric system are derived by utilizing the properties of left and right eigenvectors. To simplify the equations, the assumption is made that the mass matrix is only affected by the fluid. The simplified equation is then compared to the equation already used in ANSYS. Finally, the validity of the modal effective mass definition and derivation in this paper is demonstrated through a simple example.

비대칭 감쇠 시스템의 민감도 해석을 위한 개선된 모드법 (Modified Modal Methods for Sensitivity Analysis of Asymmetric Damped System)

  • 문영종;조지성;오주원;이인원
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2004년도 추계학술대회논문집
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    • pp.530-533
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    • 2004
  • It is well known that many real systems have asymmetric mass, damping and stiffness matrices. In this case, the method for calculating eigenpair sensitivity is different from that of symmetric system. To determine the derivatives of the eigenpairs in asymmetric damped case, a modal method was recently developed by Adhikari. When a dynamic system has many degrees of freedom, only a few lower modes are available, and because the higher modes should be truncated to use the modal method, the errors may become significant. In this paper a procedure for determining the sensitivities of the eigenpairs of asymmetric damped system using a few lowest set of modes is proposed. Numerical examples show that proposed method achieves better calculating efficiency and highly accurate results when a few modes are used.

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초음속 노즐에서 발생하는 비대칭 유동의 제어에 관한 연구 (Control of the Asymmetric Flow in a Supersonic Nozzle)

  • ;;;;;김희동
    • 한국가시화정보학회지
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    • 제9권2호
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    • pp.61-65
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    • 2011
  • Several previous works on rocket nozzle flows have revealed the existence of the transition from FSS to RSS and the occurrence of asymmetric flow associated with the boundary layer separation, which can cause excessive side-loads of the propulsion system. Thus, it is of practical importance to investigate the asymmetric flow behaviors of the propulsion nozzle and to develop its control method. In the present study, the asymmetric flow control method using a cavity system was applied to supersonic nozzle flow. Time-dependent asymmetric flow was experimentally investigated with the rate of change of the nozzle pressure ratio. The results obtained showed that the cavity system installed on nozzle wall would be helpful in fixing the unsteady motions of the boundary layer separation, consequently reducing the possibility of the occurrence of the asymmetric flow.

비대칭 감쇠 시스템의 고유진동수와 모드의 미분을 구하기 위한 모드법 의 개선 (Modified Modal Method for Eigenderivative Analysis of Asymmetric Damped System)

  • 문영종;박선규;이인원
    • 한국지진공학회:학술대회논문집
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    • 한국지진공학회 2001년도 추계 학술발표회 논문집 Proceedings of EESK Conference-Fall 2001
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    • pp.125-130
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    • 2001
  • It is well known that many real systems have asymmetric mass, damping and stiffness matrices. In this case, the method for calculating eigenpair sensitivity is different from that of symmetric system. To determine the derivatives of the eigenpairs in asymmetric damped case, a modal method was recently developed by Adhikari. When a dynamic system has many degrees of freedom, only a few lower modes are available, and because the higher modes should be truncated to use the modal method, the errors may become significant. In this paper a procedure for determining the sensitivities of the eigenpairs of asymmetric damped system using a few lowest set of modes is proposed. Numerical examples show that proposed method achieves better calculating efficiency and highly accurate results when a few modes are used.

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Reevaluating the overhead of data preparation for asymmetric multicore system on graphics processing

  • Pei, Songwen;Zhang, Junge;Jiang, Linhua;Kim, Myoung-Seo;Gaudiot, Jean-Luc
    • KSII Transactions on Internet and Information Systems (TIIS)
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    • 제10권7호
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    • pp.3231-3244
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    • 2016
  • As processor design has been transiting from homogeneous multicore processor to heterogeneous multicore processor, traditional Amdahl's law cannot meet the new challenges for asymmetric multicore system. In order to further investigate the impact factors related to the Overhead of Data Preparation (ODP) for Asymmetric multicore systems, we evaluate an asymmetric multicore system built with CPU-GPU by measuring the overheads of memory transfer, computing kernel, cache missing and synchronization. This paper demonstrates that decreasing the overhead of data preparation is a promising approach to improve the whole performance of heterogeneous system.

비대칭 감쇠 시스템의 고유진동수와 모드의 미분을 구하기 위한 모드법의 개선 (Modified Modal Method for Eigenderivative Analysis of Asymmetric Damped System)

  • 문영종;박선규;이인원
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 2001년도 가을 학술발표회 논문집
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    • pp.509-514
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    • 2001
  • It is well known that many real systems have asymmetric mass, damping and stiffness matrices. In this case, the method for calculating eigenpair sensitivity is different from that of symmetric system. To determine the derivatives of the eigenpairs in asymmetric damped case, a modal method was recently developed by Adhikari. When a dynamic system has many degrees of freedom only a few lower modes are available, and because the higher modes should be truncated to use the modal method, the errors may become significant. In this paper a procedure for determining the sensitivities of the eigenpairs of asymmetric damped system using a few lowest set of modes is proposed. Numerical examples show that proposed method achieves better calculating efficiency and highly accurate results when a few modes are used.

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편재된 비대칭형 전류고정날개 추진시스템에 관한 연구 (A Study on the Design of a Biased Asymmetric Pre-swirl Stator Propulsion System)

  • 김문찬;강용덕;전호환
    • 대한조선학회논문집
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    • 제41권3호
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    • pp.13-21
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    • 2004
  • This paper deals with a theoretical and experimental method for the design of a biased asymmetric pre-swirl stator propulsion system which is an energy saving device by recovering a propeller rotational energy. In the case of slow-speed ships, the upward flow is generated along the afterbody hull form at the propeller plane. The generated upward flow cancels the rotating flow of the propeller at the starboard part while it increases at port part. The present biased asymmetric pre-swirl stator propulsion system consists of three blades at the port and one blade at the starboard which can recover the biased rotating flow effectively. This paper provides the design concept which gives more simple and a high degree of efficiency and the experimental results for the compound propulsion system.

점성 감쇠기를 이용한 인접 비대칭 강성 구조물의 내진보강 최적설계 (Optimal Seismic Reinforcement Design of Adjacent Asymmetric-Stiffness Structures with Viscous Dampers)

  • 성은희
    • 한국안전학회지
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    • 제37권6호
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    • pp.60-70
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    • 2022
  • This paper proposes an optimal design method of a seismic reinforcement system for the seismic performance of adjacent asymmetric-stiffness structures with viscous dampers. The first method considers plan asymmetry for efficient seismic reinforcement, and evaluates the seismic performance of optimal design applied to two cases of modeling: adjacent stiffness-asymmetric structures and adjacent stiffness-symmetric structures. The second method considers the response of asymmetric structures to derive the optimal objective function, and evaluates seismic efficiency of the objective function applied to two cases of responses: horizontal displacement and torsion. Numerical analyses are conducted on 7- and 10-story structures with a uni-asymmetric-stiffness plan using six cases of historic earthquakes, normalized to 0.4g. The results indicate that the seismic performance is excellent as modeled by adjacent asymmetric-stiffness structures and how much horizontal displacement is applied as the objective function.