• Title/Summary/Keyword: NASTRAN

Search Result 393, Processing Time 0.03 seconds

다기능 복합가공기 이송시스템의 가상시제품 개발 (Development of Virtual Prototype for Multi-Purpose Lathe Slide System)

  • 정상화;차경래;김상석
    • 제어로봇시스템학회:학술대회논문집
    • /
    • 제어로봇시스템학회 2000년도 제15차 학술회의논문집
    • /
    • pp.556-556
    • /
    • 2000
  • In the multi-purpose lathe, the design of tilting turret slide system has an important and critical role to enhance the accuracy of the machining process. Tilting turret unit is traveled by 3-axis slide systems. There is a need to design this part very carefully. In this research, the 3-axis slide system with tilting turret unit is researched with two approaches; The first is that 3-axis slide system is modeled and simulated using ADAMS software. The dynamic behavior of this system is visualized by data graphs and dynamic animations. The second is that the slide system is analyzed with the aspect of stress distribution. The slide system is modeled and displayed by PATRAN and analyzed by NASTRAN. The analysis of strain and stress distribution in the each node is prompted and visualized in the computer. The first step of virtual prototype which makes it possible to design economically and effectively is developed.

  • PDF

오일러 방정식 및 저차모델링 기법을 활용한 천음속 플러터 해석 (Transonic Flutter Analysis Using Euler Equation and Reduced order Modeling Technique)

  • 김동현;김요한;김명환;류경중;황미현
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2011년도 춘계학술대회 논문집
    • /
    • pp.339-344
    • /
    • 2011
  • In the past much effort has been made to utilize advanced computational fluid dynamic (CFD) programs for aeroelastic simulations and analysis. However, it is limited in the field of unsteady aeroelasticity due to enormous size of computer memory and unreasonably long CPU time. Recently, AAEMS(Aerodynamics is Aeroelasticity minus Structure) was developed for linear time-invariant, coupled fluid-structure systems. In this paper, to demonstrate further the efficiency and accuracy of the new model reduction method, we successfully examine AGARD 445.6 wing modeled by FLUENT CFD, FSIPRO3D and NASTRAN FEM(Finite Element Method) programs. Using the ROM(Reduced Order Modeling) one can predict flutter boundary as a function of the dynamic pressure.

  • PDF

지상진동시험결과를 이용한 KC-100 항공기의 플러터 해석모델 보정 (Flutter Analysis Model Tuning of KC-100 Aircraft with the Ground Vibration Test Results)

  • 백승길;최용준
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2011년도 추계학술대회 논문집
    • /
    • pp.191-195
    • /
    • 2011
  • The airframe ground vibration tests were conducted on the KC-100 aircraft according to the regulation requirement, KAS 23.629(a)(2) and the modal characteristics for the target modes were measured. To make FE model tuning, a design sensitivity approach with engineering judgment was implemented using MSC/Nastran and Attune, a genetic algorithm based parameter optimization software. Based on the comparison between initial prediction and test results, design variables such as beam cross-sectional properties and spring stiffnesses were devised. As the results, the correlation of the FE model to the GVT results was made appropriately, meeting the goal of matching the target frequencies within 5%.

  • PDF

틸팅터릿 이송시스템의 유한요소 모델링 및 동특성 해석 (Finite element modeling and dynamic characteristic analysis of the tilting turret slide system)

  • 정상화;김상석
    • 한국공작기계학회:학술대회논문집
    • /
    • 한국공작기계학회 2000년도 추계학술대회논문집 - 한국공작기계학회
    • /
    • pp.188-192
    • /
    • 2000
  • In multi-purpose lathe, the design of tilting turret slide system has an important and critical role to enhance accuracy of the machining process. Tilting turret unit is traveled by 3-axis slide systems. There is a need to design this part very carefully. In this research, 3-axis sliding system with tilting turret is modeled by considering the element dividing, material properties, and boundary conditions using MSC/PATRAN. Mode and frequency analysis of each structures such as saddle, careg, and turret are simulated by MSC/NASTRAN, for the purpose of developing the effective design. The results of mode analysis and frequency analysis are visualized with PATRAN, and the mothod which can solve the resornance problem by eigenvalues and eigenvectors of each axe is developed as well.

  • PDF

복합 굴절차의 붐과 바스켓에 대한 구조 해석 (Structural Analysis of Booms and Basket in the Multi-aerial Platform)

  • 소수현;강성수
    • 한국생산제조학회지
    • /
    • 제21권6호
    • /
    • pp.885-891
    • /
    • 2012
  • In this study, some structural analysis using 3D CAD data, material properties, load conditions and boundary conditions are carried out to evaluate structural stability of the multi-aerial platform for high-rise fire fighting and rescue. We conduct structural analysis for the upper structures such as turn table, booms and basket, by using a universal structural analysis program NASTRAN. As the results, there is local stress exceeding the yield strength, but it is able to relax stress concentration in a way such as changing thickness of the structure or making larger inertia moment in cross section of booms.

일정속도를 갖는 유체를 포함하는 곡관의 유한요소 진동해석 (Finite Element Vibration Analysis of Curved Beam Conveying Fluid of Uniform Velocity)

  • 서영수;정의봉;오준석
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2003년도 추계학술대회논문집
    • /
    • pp.285-290
    • /
    • 2003
  • A method for the dynamic analysis of curved beam conveying fluid presents. The dynamics of curved beam is based on inextensible theory and the fluid in curved beam has uniform velocity. The equations of motion of curved beam are decoupled by in-plane motion and out-of$.$Plane motion. The solutions of equations are presented by a finite element method and validate by comparing the natural frequency with analytical solution, straight beam theories and Nastran. The influence of fluid velocity on the frequency response function is illustrated and discussed.

  • PDF

단순 및 고정 지지된 Euler 보함수 성질을 갖는 다항식을 이용한 'ㄱ'형태 벽면 구조의 고유진동해석 (Free Vibration Analysis of 'ㄱ' Type Wall Structure using Polynomials having the Property of a Simple and Fixed Support Euler Beam Functions)

  • 윤덕영;박정희
    • 한국소음진동공학회논문집
    • /
    • 제24권12호
    • /
    • pp.948-953
    • /
    • 2014
  • Many studies using the assumed mode method have been found for the free vibration analysis of stiffened plate with known elastic boundary conditions. However many local structures such as tank edges and equipment foundations consist of connected structures and it is very difficult to find suitable elastic boundary conditions. In this study combined polynomials which satisfy simply and fixedly supported boundary conditions are proposed. The proposed method has been applied to tanks which bounded by bulkhead and a deck. The results of this study shows good agreements with these obtain by the FEA S/W(Patran/Nastran).

복합단면 감쇠보의 강제진동해석 (Forced Vibration Analysis of Damped Composite Beam)

  • 원성규;정의봉;배수룡
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2006년도 춘계학술대회논문집
    • /
    • pp.411-414
    • /
    • 2006
  • In this paper, the forced vibration of damped composite beam with arbitrary section was analyzed. The damping material was assumed to have either complex shear modulus or complex Young???smodulus. Damped composite beam could be modeled using beam elements with less D.O.F. rather than solid elements. Finite element method for these methods was formulated and programmed using complex values. The results of frequency responses revealed good agreement with those of NASTRAN in several beam structures.

  • PDF

유체장 변화에 따른 사각형 탱크의 진동에 관한 연구 (Case Study on Hydroelastic Vibration of Plate for Various Bounded Fluid Field)

  • 최수현;조현동;김극수
    • 한국소음진동공학회논문집
    • /
    • 제17권1호
    • /
    • pp.3-9
    • /
    • 2007
  • In this paper, a numerical case study is carried out on the hydroelastic vibration of rectangular plate with various fluid field. It is assumed that the tank wall is clamped along the plate edges. The VMM(virtual mass method) of Nastran is used for the simulation of fluid domain and calculating natural frequency of fluid-coupled structure. In this paper, natural frequencies are calculated and compared for rectangular plates with various fluid field such as infinite fluid and finite fluid, length change of finite fluid field and various fluid contacting conditions.

합체박판 기술을 적용한 고장도 경량도어 최적 설계 (Optimal Design of Lightweight High Strength Door with Tailored Blank)

  • 송세일;박경진
    • 한국자동차공학회논문집
    • /
    • 제10권2호
    • /
    • pp.174-185
    • /
    • 2002
  • The automotive industry faces many competitive challenges including weight and cost reduction to meet need for higher fuel economy. Tailored blanks offer the opportunity to decrease door weight, reduce manufacturing costs, and improve door stiffness. Optimization technology is applied to the inner panel of a door which is made by tailored blanks. The design of tailored blanks door starts from an existing door. At first, the hinge reinforcement and inner reinforcement are removed to use tailored blanks technology. The number of parts and the welding lines are determined from intuitions and the structural analysis results of the existing door. Size optimization is carried out to find thickness while the stiffness constraints are satisfied. The door hinge system is optimized using design of experiment approach. A commercial optimization software MSC/NASTRAN is utilized for the structural analysis and the optimization processes.