• Title/Summary/Keyword: 1 자유도

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Flow Characteristics around a Circular Cylinder according as the Depth from Free Surface (자유수면에 접한 원형실린더 주위의 유동계측)

  • Shon, Chang-Bae;Gim, Ok-Sok;Oh, Woo-Jun;Lee, Chang-Woo;Lee, Gyoung-Woo
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
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    • 2010.04a
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    • pp.389-391
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    • 2010
  • The Free surface influenced the wake behind a circular cylinder and its effects were investigated experimentally in a circulating water channe with the variation of water depth Instantaneous velocity fields were measured in this paper. the measured results has been compared with each other to investigate the flow characteristics of the circular cylinder's 2-dimensional section at $Re=1.0\times10^3$ using 2-frame grey level cross correlation PIV method. The flow around the circular cylinder with free surface affected the wake structure. especially, in case of d=1.0D, the boundary layer was measured in the whole area. The separation point and boundary layer of the circular cylinder could be controlled by the water depth.

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Implementation of Airborne Multi-Function Radar Including Attitude Maneuvering (자세 기동을 고려한 항공기 탑재 다기능 레이다 통합 시뮬레이터 구현)

  • Ko, Jae-Youl;Park, Soon-Seo;Choi, Han-Lim;Ahn, Jae-Myung;Lee, Sung-Won;Lee, Dong-Hui;Yoon, Jung-Suk
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.28 no.3
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    • pp.225-236
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    • 2017
  • In this paper, a simulation test bed is presented which operates to provide full-scale simulation of airborne multi-function phased array radars. This simulation test bed provides a capability to evaluate the target tracking performance. To realize aircraft operation scenario, we developed 6DOF aircraft dynamics model which can generate trajectories and attitude of an aircraft. This procedure includes steady state flight trim search, autopilot design, and aircraft guidance command design. Also, the radar-environment integrated simulator includes target detection/measurement model and tracking filter. Developed simulator is validated by creating an air-to-air scenario.

Free Vibration of Three-Dimensional Laminated Composite Structures with Different Embedded Delamination Sizes and Locations (내재된 층간분리의 크기 및 위치 변화에 대한 3차원 복합소재 적층 구조의 자유 진동 특성)

  • Noh, Myung-Hyun;Park, Dae-Yong;Lee, Sang-Youl
    • Journal of the Korean Society for Advanced Composite Structures
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    • v.3 no.1
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    • pp.1-7
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    • 2012
  • This study investigates free vibration characteristics of laminated composite structures with different embedded delamination sizes and locations using the solid element. The three-dimensional finite element (FE) delamination model described in this paper, in comparison with the conventional approaches, is more attractive not only because it shows better accuracy but also it shows the entire mode shape. The FE model using ABAQUS is used for studying free vibrations of laminates containing an various embedded delamination. The numerical results obtained are in good agreement with those reported by other investigators. In particular, new results reported in this paper are focused on the significant effects of the local vibration mode for various parameters, such as size of delamination, aspect ratio, and location of delamination.

Study of Sloshing Flow in a Rectangular Tank (사각용기의 슬로싱 유동에 관한 연구)

  • Ji, Young-Moo;Shin, Young-Seop;Park, Jun-Sang;Hyun, Jae-Min
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.35 no.6
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    • pp.617-624
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    • 2011
  • The two-dimensional sloshing problem in a rigid rectangular tank with a free surface is considered. The flow is generated by a container in harmonic motion in time along the horizontal axis, i.e., a container excited by u=Asin($2{\pi}ft$) where u denotes the container velocity imposed externally, A is the amplitude of the oscillation velocity, and f is the frequency of oscillation. Experimental apparatus is arranged to investigate the large-amplitude sloshing flows in off-resonant conditions, where the large amplitude means that A~O(1), and the distance, S, is comparable to the breadth, L, of the container, i.e., L/S~O(1). Comprehensive particle image velocimetry (PIV) data are obtained, which show that the flow physics of the nonlinear off-resonant sloshing problem can be characterized into three peculiar free surface motions: standing-wave motions similar to those of linear sloshing, a run-up phenomenon along the vertical sidewall at the moment of turn-over of the container, and gradually propagating bore motion from the sidewall to the interior fluid region, like a hydraulic jump.

A Study on the Dynamic Wheel Loads of 3-D Vehicle Model Considering Tire Enveloping (타이어 접지폭을 고려한 3차원 차량모델에 의한 동적 차륜하중에 관한 연구)

  • Chung, Tae Ju
    • Journal of Korean Society of Steel Construction
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    • v.14 no.1
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    • pp.95-104
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    • 2002
  • In this paper, research for dynamic wheel loads of 3-D vehicle model considering tire enveloping model is carried out. Heavy trucks with 2-axles and 3-axles are modeled by 7-d.o.f. and 8-d.o.f., in which contact length of tire and pitching of tandem spring axles is considered. Dynamic equations of vehicle are derived by using the Lagrange's equation and solution of the equation is calculated by 5th Runge-Kutter method. The validity of the developed 3-D vehicle model is demonstrated by comparing the results obtained by the present method and experimental data by Whittemore. The maximum impact factors of tire force are calculated when vehicle models of 8ton and 15ton dump truck are running on the different class roads with 1.0km and on the various step bump.

Studies of Interface Continuity in Isogeometric Structural Analysis for Multi-patch Shell Components (다중 패치 쉘 아이소 지오메트릭 해석의 계면 연속성 검토)

  • Ha, Youn Doh;Noh, Jungmin
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.31 no.2
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    • pp.71-78
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    • 2018
  • This paper presents the assembling of multiple patches based on the single patch isogeometric formulation for the shear deformable shell element given in the previous study. The geometrically exact shell formulation has been accomplished with the shell theory based formulation and the generalized curvilinear coordinate system directly derived from the given NURBS geometry. For the knot elements matching across adjacent surfaces, the zero-th and first parametric continuity conditions are considered and the corresponding coupling constraints are implemented by a master-slave formulation between adjacent patches. The constraints are then enforced by a substitution method for condensation of the slave variables, thereby reducing the model size. Through numerical investigations, the important features of the first parametric continuity condition are confirmed. The performance of the multi-patch shell models is also examined comparing the rate of convergence of response coefficients for the zero and first order continuity conditions and continuity in coupling boundary between two patches is confirmed.

3-Dimensional Path Planning and Guidance using the Dubins Curve for an 3-DOF Point-mass Aircraft Model (Dubins 곡선을 이용한 항공기 3자유도 질점 모델의 3차원 경로계획 및 유도)

  • O, Su-Hun;Ha, Chul-Su;Kang, Seung-Eun;Mok, Ji-hyun;Ko, Sangho;Lee, Yong-Won
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.24 no.1
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    • pp.1-9
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    • 2016
  • In this paper, we integrate three degree of freedom(3DOF) point-mass model for aircraft and three-dimensional path generation algorithms using dubins curve and nonlinear path tracking law. Through this integration, we apply the path generation algorithm to the path planning, and verify tracking performance and feasibility of using the aircraft 3DOF point-mass model for air traffic management. The accuracy of modeling 6DOF aircraft is more accurate than that of 3DOF model, but the complexity of the calculation would be raised, in turn the rate of computation is more likely to be slow due to the increase of degree of freedom. These obstacles make the 6DOF model difficult to be applied to simulation requiring real-time path planning. Therefore, the 3DOF point-mass model is also sufficient for simulation, and real-time path planning is possible because complexity can be reduced, compared to those of the 6DOF. Dubins curve used for generating the optimal path has advantage of being directly available to apply path planning. However, we use the algorithm which extends 2D path to 3D path since dubins curve handles the two dimensional path problems. Control law for the path tracking uses the nonlinear path tracking laws. Then we present these concomitant simulation results.

Development of CMG-Based Attitude Control M&S Software (제어모멘텀휠 기반 자세제어 M&S 소프트웨어 개발)

  • Mok, Sung-Hoon;Kim, Taeho;Bang, Hyochoong;Song, Taeseong;Lee, Jongkuck;Song, Deokki;Seo, Joongbo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.47 no.4
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    • pp.289-299
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    • 2019
  • Attitude control modeling and simulation (M&S) can be extensively applied in overall development process, from simple algorithm design to on-board software verification. This paper introduces CMG-based attitude control M&S software, which consists of 6-DOF modeling (CMG and space environments modeling), and attitude control algorithm. The M&S software is divided into three modules, from an inner CMG motor control module to an outer earth observation mission module. While an application of this developed software is currently limited to the initial-phase attitude controller development, its application area can be extended to the later-phases by considering sophisticated model information in future.

Chitosan-electrolyte Complex (키토산-전해질 콤플렉스)

  • 손태원;이광순
    • Polymer Science and Technology
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    • v.15 no.3
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    • pp.334-341
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    • 2004
  • 고분자 콤플렉스 (polymer complex)는 두 개 또는 그 이상의 상호 보완적인 전하를 띄는 고분자의 조합에 의해서 형성된다. 이러한 콤플렉스는 정전기적인 힘, 소수성 상호작용, 수소결합, 반데르발스힘 등 여러 힘의 조합에 의해서 일어난다. 이들 힘에 의한 콤플렉스 형성을 그림 1에 나타내었다. 고분자의 긴 사슬로 인하여, 상호보완적인 반복단위가 모여 세그먼트 콤플렉스를 형성하고, 이렇게 모인 많은 반복단위가 자유도의 손실 없이 쉽게 회합한다. (중략)

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Position Control of a Redundant Flexible Manipulator (여유자유도 유연 매니퓰레이터의 위치제어)

  • 김진수
    • Transactions of the Korean Society of Machine Tool Engineers
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    • v.10 no.3
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    • pp.83-89
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    • 2001
  • In this paper, we discuss the vibration suppression control of spatial redundant flexible manipulators through pseudo-inversed of Jacobian. In order to verify our method, the experiments are performed for PTP(Point To Point) motion of spa-tial flexible manipulators(1) with no redundancy(2) with one redundant DOF(degree of freedom). Finally, a comparison between these results is presented to show the performance of out approach.

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