• Title/Summary/Keyword: 과도 동역학

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Analysis of Dynamic Characteristics of Fluidic Thrust Vector Control for the Over-expanded Supersonic Jet (과팽창 초음속제트의 방향 제어를 위한 유체역학적 제어의 동특성 연구)

  • Heo, Jun-Young;Yoo, Kwang-Hee;Cho, Min-Kyung;Sung, Hong-Gye;Lee, Yeol;Jeon, Young-Jin;Cho, Seung-Hwan
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.05a
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    • pp.123-127
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    • 2009
  • The purpose of this research is to investigate the dynamic characteristics of fluidic thrust vector control using the co-flow injection. In previous research, both numerical and experimental approaches for steady state were conducted to investigate operation-parameters and detail flow structure of the fluidic thrust vector control system. Based upon the previous results, numerical unsteady calculation was conducted to analyze the dynamic characteristics of jet up- and down-ward vectoring so that the transition time and the pressure distribution along the wall, and so on were investigated.

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Effects of Initial Conditions on Transient Responses in Dynamic Simulation of FOWT (초기 조건이 부유식 풍력터빈 동역학 해석의 과도응답에 미치는 영향)

  • Song, Jin-Seop;Rim, Chae-Whan;Moon, Seok-Jun;Nam, Yong-Yun
    • Journal of Ocean Engineering and Technology
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    • v.28 no.4
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    • pp.288-293
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    • 2014
  • The IEC standard for onshore or offshore wind turbines requires additional dummy simulations (at least 5 s) for the transient responses due to initial conditions. An increase in the dummy time causes a considerable increase in the computational cost considering multiple design spirals with several thousand design load analysis cases. A time of 30 s is typically used in practical simulations for a wind turbine design with a fixed platform. However, 30 s may be insufficient for floating offshore wind turbines (FOWT) because the platforms have lower natural frequencies, and the transient responses will last much longer. In this paper, an initial condition application algorithm is implemented for WindHydro, and the appropriate dummy simulation time is investigated based on a series of dynamic simulations of a FOWT. As a result, it is found that more than 300 s is required for the platform to have stationary motion after the initial transient responses for the FOWT under the conditions considered.

Real-time Fluid Animation using Particle Dynamics Simulation and Pre-integrated Volume Rendering (입자 동역학 시뮬레이션과 선적분 볼륨 렌더링을 이용한 실시간 유체 애니메이션)

  • Lee Jeongjin;Kang Moon Koo;Kim Dongho;Shin Yeong Gil
    • Journal of KIISE:Computer Systems and Theory
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    • v.32 no.1
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    • pp.29-38
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    • 2005
  • The fluid animation procedure consists of physical simulation and visual rendering. In the physical simulation of fluids, the most frequently used practices are the numerical simulation of fluid particles using particle dynamics equations and the continuum analysis of flow via Wavier-Stokes equation. Particle dynamics method is fast in calculation, but the resulting fluid motion is conditionally unrealistic The method using Wavier-Stokes equation, on the contrary, yields lifelike fluid motion when properly conditioned, yet the complexity of calculation restrains this method from being used in real-time applications. Global illumination is generally successful in producing premium-Duality rendered images, but is also excessively slow for real-time applications. In this paper, we propose a rapid fluid animation method incorporating enhanced particle dynamics simulation method and pre-integrated volume rendering technique. The particle dynamics simulation of fluid flow was conducted in real-time using Lennard-Jones model, and the computation efficiency was enhanced such that a small number of particles can represent a significant volume. For real-time rendering, pre-integrated volume rendering method was used so that fewer slices than ever can construct seamless inter-laminar shades. The proposed method could successfully simulate and render the fluid motion in real time at an acceptable speed and visual quality.

A Study on EASY5 Modeling for Performance Analysis of Turbofan Engine (터보팬 엔진의 성능해석을 위한 EASY5 모델링에 관한 연구)

  • 공창덕;강명철;기자영
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2002.04a
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    • pp.29-30
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    • 2002
  • 본 연구에서는 Boeing사에서 개발한 EASY5 프로그램을 이용하여 터보팬 엔진을 모델링하고 성능해석을 수행하였다. 연구대상 엔진인 BR715-56 엔진은 추력이 20,000lbf급인 2 스풀 터보팬 엔진으로 분리흐름(Separate Flow) 형이다. 엔진은 팬, 압축기, 연소기, 저압터어빈, 압축기터어빈, 팬 노즐 및 Core 노즐로 구성되어 있으며 Station No.는 Fig 1과 같다. 연구에 사용된 EASY5 프로그램은 동역학 시스템을 모델링하고 해석하는 프로그램으로, 제공되는 라이브러리 구성품을 이용하여 보다 쉽게 동적 시스템을 모델링할 수 있다. 또한 Steady-State Solver를 이용하여 정적 평형상태를 빠른 시간에 찾을 수 있어 보다 빠른 해석을 수행할 수 있다. 또한 해석된 동역학 모델을 FORTRAN이나 C 코드로 생성하여 제공함으로써 프로그램의 수정이나 보완이 용이하고, 제공되지 않은 시스템의 라이브러리 구성품의 경우에는 사용자 정의 코드를 만들어 사용함으로써 프로그램의 기능을 확장할 수 있다. EASy5는 대표적인 제어기 설계 소프트웨어인 MATLAB, MATRIX-x와의 호환도 가능하며 NASTRAN등과 같은 유한요소 해석 프로그램과의 데이터 공유도 가능하여 보다 폭 넓은 시스템 모델링과 제어기 설계도 쉽게 할 수 있다.

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Waveform Relaxation Method for Reactor Transient Analysis (원자로 천이해석을 위한 파형완화법)

  • Park, Keon-Woo;Co, Nam-Zin
    • Nuclear Engineering and Technology
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    • v.27 no.6
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    • pp.845-852
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    • 1995
  • We investigate the concurrent solution of differential equations by the waveform relaxation (WR) method, an iterative method for analyzing linear and nonlinear dynamical systems in the time do-main. The method, at each iteration, decomposes the dynamical system into several subsystems, each of which is analyzed for the entire given time interval. The method, when efficiently implemented, results in algorithms with a highly parallelizable concurrent fraction. In this paper, the waveform relaxation method is introduced and applied to two types of reactor dynamics problems. It is concluded that the U method can be applied to reactor dynamics equations, but that its parallel performance on the KMRR dynamics is only modest.

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Rotordynamic Analysis of a High Thrust Liquid Rocket Engine Turbopump (고추력 액체 로켓 엔진용 터보펌프의 회전체동역학 해석)

  • Jeon, Seong-Min;Kwak, Hyun-Duck;Yoon, Suk-Hwan;Kim, Jin-Han
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.36 no.7
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    • pp.688-694
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    • 2008
  • A rotordynamic analysis is performed for a high thrust class liquid rocket engine turbopump considering the dynamic characteristics of ball bearings and pump noncontact seals. Complex eigenvalue problems are solved to predict the rotating natural frequencies and damping ratios as a function of rotating speeds. Synchronous rotor mass unbalance response and time transient response analyses are also performed to figure out the rotor critical speed and the onset speed of instability. From the numerical analysis, it is found that the rear bearing stiffness is most important parameter for the critical speed and instability because the 1st mode is turbine side shaft bending mode. The pump seal effect on the critical speed is enlarged as the rear bearing stiffness decreases and the front bearing stiffness increases.

Multi-body dynamics simulation of 14 facepieces and probability study by using residual moment (14 면체의 다물체 동역학 Simulation 과 잔류 모멘트 계산을 통한 확률계산)

  • Lee, Jeong-Han;Yoo, Wan-Suk
    • Proceedings of the KSME Conference
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    • 2008.11a
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    • pp.865-869
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    • 2008
  • Juryeonggu is a Cuboctahedral die that had used in ancient Korea. This Cuboctahedral is consisted of different two penal servitudes of 14 facepieces, but the probability distribution can appear equally so it can be usable as a die. In this paper, achieved research study about probability of a Cuboctahedral die that have quadrilateral and triangle preferentially to search Juryeonggu's probability calculation method. First, confirmed probability distribution through Multibody-dynamics analysis and verified probability distribution through several experiments. Finally, with this simulation data, achieved theoretical analysis about Cuboctahedral die occurrence probability by using the residual momentum energy.

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공작기계 이송계의 동적 시뮬레이션 모델의 개발

  • 정영훈;민병권;조동우
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2004.05a
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    • pp.319-319
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    • 2004
  • 최근 컴퓨터 기술의 급속한 발전과 함께, 생산품질의 향상과 생산주기의 단축을 목적으로 유한요소법(FEM)과 다물체 동역학(multi-body dynamics)과 같은 시뮬레이션 기술(math-based engineering)이 산업계 전반에 폭넓게 적용되고 있다. 생산시스템 분야에서는 디지털 생산기술(digital manufacturing) 및 가상 생산기술(virtual manufacturing)의 개념이 소개되면서 생산시스템의 모델링 및 시뮬레이션에 관한 연구가 활발히 시도되고 있다. 그러나 아직까지 대부분의 시뮬레이션 기술이 구조해석과 같은 제한적으로 부문에서만 활용되고 있는 실정이며, 시뮬레이션 모델은 대상이 되었던 몇몇 특수한 경우에 제한적으로 사용될 수 있는 등의 한계를 보여 왔다.(중략)

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Application of Neural Networks in Robot Dynamics Control (로봇 동역학 제어를 위한 인공신경회로망 적용 연구)

  • 조용중;이상훈;송지혁;이성범;김상우;오세영
    • Proceedings of the Korean Information Science Society Conference
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    • 2000.10b
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    • pp.326-328
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    • 2000
  • 인공신경회로망 기술은 선형 또는 비선형성 계산 문제를 복잡도에 무관하게 학습에 의해 자동으로 근사한다. 또한 알고리즘이 단순하며 잡음에 강하여 다양한 분야에 적용되고 있다. 반면 대상시스템의 특성이나 조건이 변경되면 계산성능을 보장할 수 없고, 계산의 신뢰성 보장 한계가 모호하기 때문에 제어문제에는 실용화가 어려운 것으로 알려져 있다. 제안 모델은 인공신경회로망의 장점을 유지하면서, 위와 같은 문제점을 해결한다. 시뮬레이션을 통하여 제안 모델은 기존 제어기에 비해 우수한 추종제어성능을 보이는 것으로 밝혀졌다.

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