• 제목/요약/키워드: ANSYS/Multiphysics

검색결과 9건 처리시간 0.028초

LNG 벙커링용 QC/DC 밸로즈의 유동/구조 해석 (CFD/CAE Analysis of QC/DC Bellows for LNG Bunkering)

  • 장성철;엄정필;정현철
    • 한국산업융합학회 논문집
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    • 제21권5호
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    • pp.191-195
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    • 2018
  • By using an ANSYS product suite (CFX, Ansys Multiphysics), which is a powerful tool for multiphysics analysis of complicated physical phenomena, we performed a structural stress analysis based on fluid flow and heat transfer phenomena within a quick connect/disconnect (QC/DC) bellows system. Considering the extremely low temperatures in the QC/DC environment, an approach to the problem based on complex multi-physics phenomena, where different phenomena interact with each other, is crucial. Therefore, we use a numerical analysis technique where fluid-thermal-structural interactions are combined. In conclusion, when low temperature fluids flow inside bellows, the expected service life is conspicuously reduced due to the thermal stress caused by heat transfer. Therefore, in future research, a structure with considerably reduced thermal stress by robust design optimization will be derived.

Topology Optimization of the Decking Unit in the Aluminum Bass Boat and Strength Verification using the FEM-program

  • Seo, Kwang-Cheol;Gwak, Jin;Park, Joo-Shin
    • 해양환경안전학회지
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    • 제24권3호
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    • pp.367-372
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    • 2018
  • The objective of this paper is to optimize the cross-section of aluminum decking units used in the bass boats under operating conditions, and to verify the optimized model from the results via by ANSYS software. Aluminum decking unit is needed to endure specific loading while leisure activity and sailing. For a stiffer and more cost-neutral aluminum decking unit, optimization is often considered in the naval and marine industries. This optimization of the aluminum decking unit is performed using the ANSYS program, which is based on the topology optimization method. The generation of finite element models and stress evaluations are conducted using the ANSYS Multiphysics module, which is based on the Finite Element Method (FEM). Through such a series of studies, it was possible to determine the most suitable case for satisfying the structural strength found among the phase-optimized aluminum deck units in bass boats. From these optimization results, CASE 1 shows the best solution in comparison with the other cases for this optimization. By linking the topology optimization with the structural strength analysis, the optimal solution can be found in a relatively short amount of time, and these procedures are expected to be applicable to many fields of engineering.

드라이도크 게이트의 설계 및 구조해석 (Design and Structural Analysis of Dry Dock Gate)

  • 박주신;안환진;정길용
    • 해양환경안전학회지
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    • 제14권4호
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    • pp.325-331
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    • 2008
  • 최근 조선산업의 호황으로 인하여, 신생 조선소들이 많이 설립되고 있다. 이러한 조선소의 설비상의 특징은 기존의 조선소에 비해 규모가 크며, 또한 진수방식을 대형조선의 방식인 드라이도크 진수를 채택하고 있다. 본 연구 논문에서는 드라이도크 게이트의 구조 설계 및 유한요소법을 적용한 구조해석에 대해서 나타내고 있다. 설계는 트라이본을 사용하였고, 구조강도 평가는 범용 유한요소 해석 프로그램인 ANSYS Multiphysics 모듈을 이용하여 계산하였다. 드라이도크 게이트는 자주 개폐를 하지 않으며, 도크내에서 일정한 건조 기간동안 외부의 해수압을 견딜 수 있는 구조 강도를 갖고 있어야만 한다. 실제적으로, 이 구조물의 설계 및 구조강도 평가에 대한 자료는 거의 찾아볼 수가 없어서, 설계 기준 및 합리적인 구조강도 평가에 대한 기준이 필요시 되고 있다. 향후 이러한 구조물의 설계 및 구조강도 평가에 본 연구논문은 기초적인 자료 및 참고문헌으로 유익하게 사용되리라고 판단된다.

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Acoustic responses of natural fibre reinforced nanocomposite structure using multiphysics approach and experimental validation

  • Satankar, Rajesh Kumar;Sharma, Nitin;Ramteke, Prashik Malhari;Panda, Subtra Kumar;Mahapatra, Siba Shankar
    • Advances in nano research
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    • 제9권4호
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    • pp.263-276
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    • 2020
  • In this article, the acoustic responses of free vibrated natural fibre-reinforced polymer nanocomposite structure have been investigated first time with the help of commercial package (ANSYS) using the multiphysical modelling approach. The sound relevant data of the polymeric structure is obtained by varying weight fractions of the natural nanofibre within the composite. Firstly, the structural frequencies are obtained through a simulation model prepared in ANSYS and solved through the static structural analysis module. Further, the corresponding sound data within a certain range of frequencies are evaluated by modelling the medium through the boundary element steps with adequate coupling between structure and fluid via LMS Virtual Lab. The simulation model validity has been established by comparing the frequency and sound responses with published results. In addition, sets of experimentation are carried out for the eigenvalue and the sound pressure level for different weight fractions of natural fibre and compared with own simulation data. The experimental frequencies are obtained using own impact type vibration analyzer and recorded through LABVIEW support software. Similarly, the noise data due to the harmonically excited vibrating plate are recorded through the available Array microphone (40 PH and serial no: 190569). The numerical results and subsequent experimental comparison are indicating the comprehensiveness of the presently derived simulation model. Finally, the effects of structural design parameters (thickness ratio, aspect ratio and boundary conditions) on the acoustic behaviour of the natural-fibre reinforced nanocomposite are computed using the present multiphysical model and highlighted the inferences.

수중추진기의 추진력 시뮬레이션 및 실험 (Thrust Simulation and Experiments for Underwater Thrusters)

  • 안용석;백운경
    • 동력기계공학회지
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    • 제21권3호
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    • pp.51-59
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    • 2017
  • In the early design stage of underwater vehicles, it is important to estimate the vehicle's underwater motion performance. The key design elements for the motion are propellers, battery power, and underwater resistance of the vehicle. Small thrusters with motor and propeller are usually used for the UUV(unmanned underwater vehicles). In this study, a multiphysics thruster model combining electro-mechanical and hydrodynamics characteristics was proposed to estimate the thruster performance. To show the applicability of the mathematical model, an sample thruster was used for the derive the unknown parameters of thruster. Hydrodynamic parameters were calculated for a 3D geometry model of the propeller by ANSYS/CFX program. Finally, Matlab/simulink program was used for the numerical simulation to predict the thruster performance from the given voltage/current input to the motor. Also, proved validity of simulation model by experiment test. Test were done by 2 mode(middle/high speed, reverse). The thruster performance curves obtained from this simulation were confirmed to be similar with experiment results.

진공차단부에서 발생하는 확산형 아크 수치해석 (Numerical Study on a Diffused-mode Arc within a Vacuum Interrupter)

  • 조성훈;황정훈;이종철;최명준;권중록;김윤제
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 춘계학술대회논문집
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    • pp.479-482
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    • 2008
  • In order to more closely examine the vacuum arc phenomena, it is necessary to predict the magnetohydrodynamic (MHD) characteristics by the multidisciplinary numerical modeling, which is coupled with the electromagnetic and hydrodynamic fields, simultaneously. In this study, the thermal-fluid characteristics of high current vacuum arcs were calculated by a commercial multiphysics package, ANSYS, in order to obtain Joule heat, Lorentz force and the interactions with flow variables. We assumed the diffused-mode arc within an AMF vacuum interrupter. It was found with four different currents that the temperature distributions on the anode surface are diffused uniformly without concentration in 7kA for both types (cup and coil-type). But the arc plasma transition and an increase of thermal flux density for increasing the applied current have caused the change of temperature distributions on the anode surface. We should need further studies on the two-way coupling method and radiation model for arc plasmas in order to accomplish the advanced analysis method for multiphysics.

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순차적 전자기-구조 연성해석을 통한 전자기성형 공정 해석 (Analysis of Electromagnetic Forming Using Sequential Electromagnetic-Mechanical Coupled Simulations)

  • 김정;노학곤;고세진;김태정
    • 소성∙가공
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    • 제21권7호
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    • pp.441-446
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    • 2012
  • A sequential coupled field analysis of electromagnetic free bulging was performed by using FEM. A 2D axi-symmetric electromagnetic model based on the magnetic vector potential is proposed for the calculation of magnetic field and Lorentz's forces. The Newmark integration method is used to calculate the transient dynamic plastic deformation of sheet during free bulging. In the finite element model, the effect of sheet deformation on the electromagnetic field analysis is taken into consideration. In order to confirm the sequential electromagnetic-mechanical coupling analysis, an experiment with an electromagnetic forming apparatus was conducted. The results showed that the final bulge height of the sheet predicted from the proposed method is in good agreement with experimentally measured height.

유체 렌즈의 초점과 유동 인자의 상관관계에 대한 수치해석 (Numerical study on the relation between flow parameters and the focal point of fluidic lens)

  • ;김대겸
    • 한국가시화정보학회지
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    • 제17권2호
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    • pp.90-95
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    • 2019
  • In the present work, the effect of flow parameters such as volume flow rate on focal point of fluidic micro lens is investigated numerically. ANSYS Fluent is used for simulations, and the flow parameters and number of simulations are determined using the space filling method of design of experiment (DOE). Having determined the location of interfaces between fluids inside the micro lens which acts as the lens curvature, a ray tracking simulation on each case is performed using COMSOL Multiphysics to determine the focal point for each lens. These data are then used to provide a relation between flow parameters and the focal point of the lens.

비행 시나리오에 따른 FSS 레이돔의 전파 투과 특성 변화 분석 (Analysis on Change in Electrical Transmission Characteristic about FSS Radome on Flight Scenario)

  • 김선휘;배형모;김지혁;이남규;남주영;박세진;조형희
    • 한국추진공학회지
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    • 제23권6호
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    • pp.11-20
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    • 2019
  • 레이돔은 레이더를 외부 환경으로부터 보호하는 역할을 하며, 스텔스 기술의 일환으로 주파수 선택 표면이 레이돔에 적용되고 있다. 본 연구에서는 Jerusalem-cross(JSC) 형상이 적용된 주파수 선택 표면 레이돔에 대해 비행 시나리오 상 공력가열로 인해 미사일의 FSS 레이돔의 전파 투과 특성의 변화를 다루었다. 이 내용을 바탕으로 공력가열에 따른 전파 투과 특성을 레이돔의 위치에 따라, 시간에 따라 수치 해석적으로 분석하였다. 수치 해석적 연구로 상용 프로그램 ANSYS Fluent 15.0과 COMSOL Multiphysics 5.2를 사용하였다. 비행 시나리오 상 전파 투과 특성의 변화로 초기 대역폭에 대한 평균 투과율 수치가 최대 -14.3 dB까지 변화하는 것을 확인할 수 있었다.