• Title/Summary/Keyword: structural requirement

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Trial Design of a Very Large Floating Airport (General Arrangement and Decision of Depth) (초대형 부유식 해상공항의 시설계 (일반배치와 깊이 결정))

  • 신현경;임춘규;정재희
    • Proceedings of the Korea Committee for Ocean Resources and Engineering Conference
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    • 2001.10a
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    • pp.45-49
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    • 2001
  • The length and the breadth or a very large floating airport are determined by airplane types and airport facilities. However, the depth affect not only the structural strength but also the functional requirement such as a possibility of taking off and landing. The optimization problem for determining the depth is to select a design so that the cost is minimized. In this paper, a general arrangement and a method to decide the depth are proposed. Strength, functional requirement, and possibility of occurrence of deck wetness and slamming are considered in order to determine the depth of structure. Hydrodynamic forces of the diffraction and radiatin problems are predicted by applying the source-dipole distribution method, and the structural responses are obtained by the finite element method.

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Performance based design optimum of CBFs using bee colony algorithm

  • Mansouri, Iman;Soori, Sanaz;Amraie, Hamed;Hu, Jong Wan;Shahbazi, Shahrokh
    • Steel and Composite Structures
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    • v.27 no.5
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    • pp.613-622
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    • 2018
  • The requirement to safe and economical buildings caused to the exploitation of nonlinear capacity structures and optimization of them. This requirement leads to forming seismic design method based on performance. In this study, concentrically braced frames (CBFs) have been optimized at the immediate occupancy (IO) and collapse prevention (CP) levels. Minimizing structural weight is taken as objective function subjected to performance constraints on inter-story drift ratios at various performance levels. In order to evaluate the seismic capacity of the CBFs, pushover analysis is conducted, and the process of optimization has been done by using Bee Algorithm. Results indicate that performance based design caused to have minimum structural weight and due to increase capacity of CBFs.

Planar Structural Requirement at 4-position of 1-Arylsulfonyl-4-phenyl-4,5-dihydro-2-imidazolones for their Cytotoxicity

  • Jung, Sang-Hun;Kwak, Suhk-Jun
    • Archives of Pharmacal Research
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    • v.20 no.3
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    • pp.283-287
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    • 1997
  • In order to identify the structural requirement at 4-position of 1-arylsulfonyl-4-phenyl-4,5-dihydro-2-limidazolones 3 for their cytotoxicity, the corresponding 1-arylsulfonyl-4-cyclohexyl-4,5-dihydro-2-imidazolones 4 were synthesized and their in vitro cytotoxicity against human solid tumor cell lines were measured. Unlike compounds 3a-c, cyclohexyl analogues 4a-c do not show the cytotoxicity. This dramatic loss of activity of these analogues on the volume change with the bulkier cyclohexyl group indicates that the planar structure at 4-position of 1-arylsulfonyl-4-pheny-4,5-dihydro-2-limidazolones 3 is required for their activity as an important pharmacophoric moiety.

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Structural Requirement of New Chalcones for the Inhibitory Activity of Interleukin-5

  • Cho, Soo-Hyun;Yang, Hyun-Mo;The, Hung-Dang;Ju, Jung-Hun;Kim, Mi-Kyung;Lee, Seung-Ho;Ryu, Jae-Chun;Kim, Young-Soo;Jung, Sang-Hun
    • Proceedings of the PSK Conference
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    • 2003.04a
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    • pp.233.1-233.1
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    • 2003
  • Interleukin (IL)-5 appears to be one of the main proinflammatory mediators among a growing number of cytokines and chemokines that induce eosinophilic inflammation. Sophoricoside and their analogs isolated from Sophora japonica show relatively potent inhibitory activity of interleukin (IL)-5 as a small molecule. Initial attempt to identify the structural requirement of this isoflavonone led to find new chalcones to exhibit the inhibitory activity of IL -5. (omitted)

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Subscale Main Wing Design and Manufacturing of WIG Vehicle Using Carbon Fiber Composites

  • Park, Hyun-Bum
    • International Journal of Aerospace System Engineering
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    • v.4 no.2
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    • pp.1-4
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    • 2017
  • This work dealt with design and manufacturing of WIG vehicle wing using carbon/epoxy composite materials. In this study, structural design and analysis of carbon composite structure for WIG craft were performed. Firstly, structural design requirement of wing for WIG vehicle was investigated. After structural design, the structural analysis of the wing was performed by the finite element analysis method. It was performed that the stress, displacement and buckling analysis at the applied load condition. And also, manufacturing of subscale wing using carbon/epoxy composite materials was carried out. After structural test of target structure, structural test results were compared with analysis results. Through the structural analysis and test, it was confirmed that the designed wing structure is safety.

Structural Design on Joint Component of Composite Wing of WIG Craft

  • Lee, Younggyu;Park, Hyunbum
    • International Journal of Aerospace System Engineering
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    • v.8 no.2
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    • pp.1-3
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    • 2021
  • This study proposed a specific preliminary structural design procedure of the main wing for a small scale WIG vehicle to meet the target weight of the system requirement. The high stiffness and strength Carbon-Epoxy material was used for lightness, and the foam sandwich type structure at the upper skin and the spar webs was adopted for improvement of structural stability. After structural design, wing joint part was designed. Through investigation on structural design result, design modification was performed. After design modification, even thought the designed wing weight was a little bit heavier than the target wing weight, the structural safety and stability of the final design feature was confirmed.

A Study on the Structural Analysis and Design of Avionics Equipment (항공전자장비의 구조해석 및 설계에 대한 연구)

  • Choi, In-Ho
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.13 no.5
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    • pp.2015-2022
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    • 2012
  • This paper is about the analysis and design of avionics equipment's housing and PCB(Printed Circuit Board) such as air data computer. Avionics equipment's structural design as well as electrical properties is very critical and should be proved from design phase by analysis method. First, analyze the static load and vibration requirement for the installed equipment, and then proved it satisfy with its requirement using the computational structural analysis. Commercial tools were used for computation and the rib design of housing was verified and the placement of electrical component was proposed using the PCB's local displacement information.

Intellectual Capital: A Review from the Literature

  • Rahman, Md. Musfiqur;Khatun, Naima
    • The Journal of Industrial Distribution & Business
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    • v.7 no.4
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    • pp.5-9
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    • 2016
  • Purpose - The purpose of this paper is to get a clear concept about intellectual capital and reports on intellectual capital in different entities based on the literature review. Research design, data, and methodology - This study was mainly written in a way of descriptive research. The current studies deal with the theoretical and reporting aspects on intellectual capital. Thus, this research is developed on the basis of previous descriptive and empirical research papers. Results - This study finds that intellectual capital is the combination of human capital, structural capital and relational capital but there is no unique measurement system or process to define intellectual capital. The findings also indicates that the measurement for intellectual capital varies based on the measurement process, time period, firms, industries and country to country perspectives. It can be also observed that firms have the tendency not to disclose the intellectual capital information. Conclusions - This study recommends that intellectual capital should be presented in a fixed format and human, relational and structural capital should be included as intellectual capital. Additionally, it suggests that mandatory requirement of legislation, effective corporate governance mechanism and stock exchange listing requirement might increase the quality of intellectual reporting.

Analyses on Thermal Stability and Structural Integrity of the Improved Disposal Systems for Spent Nuclear Fuels in Korea

  • Lee, Jongyoul;Kim, Hyeona;Kim, Inyoung;Choi, Heuijoo;Cho, Dongkeun
    • Journal of Nuclear Fuel Cycle and Waste Technology(JNFCWT)
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    • v.18 no.spc
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    • pp.21-36
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    • 2020
  • With respect to spent nuclear fuels, disposal containers and bentonite buffer blocks in deep geological disposal systems are the primary engineered barrier elements that are required to isolate radioactive toxicity for a long period of time and delay the leakage of radio nuclides such that they do not affect human and natural environments. Therefore, the thermal stability of the bentonite buffer and structural integrity of the disposal container are essential factors for maintaining the safety of a deep geological disposal system. The most important requirement in the design of such a system involves ensuring that the temperature of the buffer does not exceed 100℃ because of the decay heat emitted from high-level wastes loaded in the disposal container. In addition, the disposal containers should maintain structural integrity under loads, such as hydraulic pressure, at an underground depth of 500 m and swelling pressure of the bentonite buffer. In this study, we analyzed the thermal stability and structural integrity in a deep geological disposal environment of the improved deep geological disposal systems for domestic light-water and heavy-water reactor types of spent nuclear fuels, which were considered to be subject to direct disposal. The results of the thermal stability and structural integrity assessments indicated that the improved disposal systems for each type of spent nuclear fuel satisfied the temperature limit requirement (< 100℃) of the disposal system, and the disposal containers were observed to maintain their integrity with a safety ratio of 2.0 or higher in the environment of deep disposal.