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공기저항 저감을 위한 컨테이너선 상부구조물 형상설계 및 성능평가Design and Performance Evaluation of Superstructure Modification for Air Drag Reduction of a Container Ship

Other Titles
Design and Performance Evaluation of Superstructure Modification for Air Drag Reduction of a Container Ship
Authors
김윤식김광수정성욱정승규반석호김진
Issue Date
2015
Publisher
대한조선학회
Keywords
공기저항 저감; 컨테이너선; 풍동시험; 상부구조물; 풍하중; 전산유체역학; Air drag reduction; Container ship; Wind tunnel test; Superstructure; Wind load; Computational Fluid Dynamics
Citation
대한조선학회 논문집, v.52, no.1, pp 8 - 18
Pages
11
Journal Title
대한조선학회 논문집
Volume
52
Number
1
Start Page
8
End Page
18
URI
https://www.kriso.re.kr/sciwatch/handle/2021.sw.kriso/820
ISSN
1225-1143
Abstract
Reduction of the fuel oil consumption and corresponding greenhouse gas exhausted from ships is an important issue for today’s shipdesign and shipping. Several concepts and devices on the superstructure of a container ship were suggested and tested in the windtunnel to estimate the air drag reduction. As a preliminary performance evaluation, air drag contributions of each part of thesuperstructure and containers were estimated based on RANS simulation respectively. Air drag reduction efficiency of shapemodification and add-on devices on the superstructure and containers was also estimated. Gap-protectors between containers and avisor in front of upper deck were found to be most effective for drag reduction. Wind tunnel tests had been carried out to confirm thedrag reduction performance between the baseline(without any modification) configuration and two modified superstructure configurationswhich were designed and chosen based on the computation results. The test results with the modified configurations show considerableaerodynamic drag reduction, especially the gap-protectors between containers show the largest reduction for the wide range ofheading angles. RANS computations for three configurations were performed and compared with the wind tunnel tests. Computationresult shows the similar drag reduction trend with experiment for small heading angles. However, the computation result becomes lessaccurate as heading angle is increasing where the massively separated flow is spread over the leeward side.
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