• Title/Summary/Keyword: structural design process

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Integrated Structural Design Operation by Process Decomposition and Parallelization (프로세스 분할 병행에 의한 통합 구조설계 운용)

  • Hwang, Jin-Ha;Park, Jong-Hoi
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.21 no.1
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    • pp.113-124
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    • 2008
  • Distributed operation of overall structural design process, by which product optimization and process parallelization are simultaneously implemented, is presented in this paper. The database-interacted hybrid method, which selectively takes the accustomed procedure of the conventional method in the framework of the optimal design, is utilized here. The staged application of design constraints reduces the computational burden for large complex optimization problems. Two kinds of numeric and graphic processes are simultaneously implemented by concurrent engineering approach in the distributed environment of PC networks. The former is based on finite element optimization method and the latter is represented by AutoCAD using AutoLISP programming language. Numerical computation and database interaction on servers and graphic works on independent clients are communicated through message passing. The numerical experiments for some steel truss models show the validity and usability of the method. This study has sufficient adaptability and expandability, in that it is based on general methodologies and industry standard platforms.

A Study on the Web-based Distributed System Framework (웹 기반 분산설계 시스템에 관한 연구)

  • Yang, Young-Soon;Park, Chang-Kue;Suh, Hyo-Won;Park, Chan-Hyouk
    • Proceedings of the Computational Structural Engineering Institute Conference
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    • 2007.04a
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    • pp.707-712
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    • 2007
  • Recently, the rapid progress of Internet and Network affects engineering design environment as well as business fields to utilize Web technologies to enhance it's competitiveness in the world. This situation has also caused many companies to seek out the possibility to increase the collaboration between different organizations within their Product design process. Thus. this research shows the web based distributed design system framework which involves Workflow-based framework that enables to automate, integrate and manage the design process, such as CAD, CAE, Optimization tools.

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Gaussian models for bond strength evaluation of ribbed steel bars in concrete

  • Prabhat R., Prem;Branko, Savija
    • Structural Engineering and Mechanics
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    • v.84 no.5
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    • pp.651-664
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    • 2022
  • A precise prediction of the ultimate bond strength between rebar and surrounding concrete plays a major role in structural design, as it effects the load-carrying capacity and serviceability of a member significantly. In the present study, Gaussian models are employed for modelling bond strength of ribbed steel bars embedded in concrete. Gaussian models offer a non-parametric method based on Bayesian framework which is powerful, versatile, robust and accurate. Five different Gaussian models are explored in this paper-Gaussian Process (GP), Variational Heteroscedastic Gaussian Process (VHGP), Warped Gaussian Process (WGP), Sparse Spectrum Gaussian Process (SSGP), and Twin Gaussian Process (TGP). The effectiveness of the models is also evaluated in comparison to the numerous design formulae provided by the codes. The predictions from the Gaussian models are found to be closer to the experiments than those predicted using the design equations provided in various codes. The sensitivity of the models to various parameters, input feature space and sampling is also presented. It is found that GP, VHGP and SSGP are effective in prediction of the bond strength. For large data set, GP, VHGP, WGP and TGP can be computationally expensive. In such cases, SSGP can be utilized.

Structural Sizing for Optionally Piloted PAV Preliminary Design (유무인 겸용 개인항공기(OPPAV) 개념설계를 위한 구조물 사이징)

  • Kim, Sung Joon;Lee, Seung-gyu
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.28 no.1
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    • pp.83-89
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    • 2020
  • Personal air vehicle (PAV) is considered by aviation engineers as a solution to provide fast urban mobility. The purpose of designing a optionally piloted PAV (OPPAV) is to provide an individual air vehicle. The airframe structure is designed with high strength carbon fiber composite to reduce the aircraft weight. This paper presents an overview of sizing process for OPPAV at the conceptual design level. It consists of load analysis, structural sizing and development of efficient design allowable values for composite material. The weight is estimated based on sizing process, including strength and stiffness requirements. The objective of this study is to present a overview of structural sizing procedure and fast tool for preliminary design phases.

Derivation of design charts based on the two-dimensional structural analysis of geotextile tubes

  • Kim, Hyeong-Joo;Won, Myoung-Soo;Park, Tae-Woong;Choi, Min-Jun;Jamin, Jay C.
    • Structural Engineering and Mechanics
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    • v.55 no.2
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    • pp.349-364
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    • 2015
  • Analytical solutions for modeling geotextile tubes during the filling process and approximation method to determine the densified tube shape are reviewed. The geotextile tube filling analysis is based on Plaut & Suherman's two-dimensional solution for geotextile tubes having a weightless and frictionless inextensible membrane resting on a rigid horizontal foundation subjected to internal and external hydrostatic pressures. The approximation for the densified tube shape developed by Leshchinsky et al. was adopted. A modified method for approximating the densified tube shape based on an areal-strain deformation analysis is introduced. Design diagrams useful for approximating geotextile tube measurements in the design process are provided.

A Study on the Structural Integrity of Lifting Lug without Appendage (부가물이 미부착된 리프팅 러그의 구조 건전성에 관한 연구)

  • Choi, Kyung-Shin;Kim, Ji-Jun;Choi, JeongJu
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.20 no.11
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    • pp.108-114
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    • 2021
  • In this study, a multivariate function was applied to the genetic algorithm for D-type lugs currently used in shipyards to closely analyze the behavioral form of weight loss without double plates. An optimal lifting lug structure design without attachments is proposed. MATLAB R2016a was used to design features by applying multivariate functions to genetic algorithms. Furthermore, the design was achieved by deriving the optimal shapes of lugs using genetic algorithms. The shapes of the designed lugs were validated for structural bonding using the structural analysis program ANSYS 2020 R2, and a robust design of lugs with no appendages was developed.

Structural Design for 2kW Class Wind Turbine Blade by using Design of Experiment (실험계획법을 이용한 2kW급 풍력발전용 블레이드에 대한 구조설계)

  • Lee, Seung-Pyo;Kang, Ki-Weon;Chang, Se-Myong;Lee, Jang-Ho
    • Journal of the Korean Society of Manufacturing Technology Engineers
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    • v.20 no.1
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    • pp.28-33
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    • 2011
  • In this paper, structural design for 2kW class composite blade is performed by using design of experiment(DOE). A full factorial design is applied to meet the design specifications at the manufacturing process. The analysis of variance(ANOVA) is made in order to determine the significance of effects in an analysis. Structural analysis by using of commercial software ABAQUS is performed to compute the displacement and safety factor of filament wound composite blade. The results show that the proposed method is suitable to analyze the factors at the design of wind turbine blade.

Measurements on the Characteristics of Dynamic and Vertical Vibration Transfer according to floors of Building Structures using Accelerometer and Dynamic signal analyzer (가속도계와 동적신호분석기를 이용한 건축물 바닥슬래브 동특성 및 수직진동 전달특성 측정)

  • Chun Ho-Min
    • Proceedings of the Computational Structural Engineering Institute Conference
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    • 2006.04a
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    • pp.29-34
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    • 2006
  • In general, the vertical vibration problems for .strength of members and serviceability of building structures are not considered in structural design process, but the prediction of the vertical vibration is very important and essential to structural design process. This study aims to investigate the characteristics of vertical vibration in terms of the transfer of horizontal directions on the rahmen building structures. In order to examine the characteristics of vertical vibration, the modal test and the impact (heel-drop and hammer) excitation experiments were conducted several times on three building structures. The results from the experiments are analyzed and compared. with the results. The results of this study suggest that the characteristics of vertical vibration transfer in horizontal way are effected from the fundamental frequency of the slabs and excitation forces.

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A Study on the Structure Analysis of Riveting Process for Aircraft Frame Manufacturing (항공기 프레임 제작을 위한 리벳팅 공정의 구조해석에 관한 연구)

  • Lee, Choon-Man;Oh, Won-Jung
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.19 no.2
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    • pp.103-110
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    • 2020
  • Riveting is mainly used to assemble the aircraft fuselage. An average of 2~3 workers is needed to assemble an aircraft fuselage consisting of various size frames by riveting. In this study, a riveting process that enables one-person operation using an automated C-frame riveting machine was proposed for improving the efficiency of productivity. The proposed process was verified stability through structural analysis. In the range that can maintain structural stability, panel thickness of the riveting machine and shape were modified to optimizing the shape for reducing the weight of the riveting process. The structural analysis was performed by software ANSYS workbench 19.2. The optimized riveting machine was reduced by 257kg compared to the existing model.

Backward Extrusion Process Analysis and Ductile Fracture Minimization of Titanium (티타늄합금의 후방압출 공정해석 및 연성파괴 최소화)

  • 신태진;이유환;이종수;황상무
    • Proceedings of the Korean Society for Technology of Plasticity Conference
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    • 2003.05a
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    • pp.351-354
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    • 2003
  • Titanium alloys are a vital element for developing advanced structural components, especially in aerospace applications. However, process design for successful forming of titanium alloy is a difficult task, which is to be achieved within a very narrow range of process parameters. Presented in this paper is a finite element - based optimal design technique as applied to ductile fracture minimization process design in backward extrusion of titanium alloys.

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