• Title/Summary/Keyword: Substantiation Test

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Collision-Damage Analysis of a Floating Offshore Wind Turbine Considering Ship-Collision Risk

  • Young-Jae Yu;Sang-Hyun Park;Sang-Rai Cho
    • Journal of Ocean Engineering and Technology
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    • v.38 no.3
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    • pp.124-136
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    • 2024
  • As the number of offshore wind-power installations increases, collision accidents with vessels occur more frequently. This study investigates the risk of collision damage with operating vessels that may occur during the operation of an offshore wind turbine. The floater used in the collision study is a 15 MW UMaine VolturnUS-S (semi-submersible type), and the colliding ships are selected as multi-purpose vessels, service operation vessels, or anchor-handling tug ships based on their operational purpose. Collision analysis is performed using ABAQUS and substantiation is performed via a drop impact test. The collision analyses are conducted by varying the ship velocity, displacement, collision angle, and ship shape. By applying this numerical model, the extent of damage and deformation of the collision area is confirmed. The analysis results show that a vessel with a bulbous bow can cause flooding, depending on the collision conditions. For damage caused by collision, various collision angles must be considered based on the internal stiffener arrangement. Additionally, the floater can be flooded with relatively small collision energy when the colliding vessel has a bulbous bow.

Quantitive Evaluation of Reproducibility of Embankment for Full Scale Test through Statistical Analysis of Physical Properties of Soil (지반물성치 통계분석을 통한 실규모 시험용 제방축조의 재현성에 관한 정량적 평가)

  • Lee, Heemin;Moon, Junho;Kim, Minjin;Kim, Younguk
    • Journal of the Korean GEO-environmental Society
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    • v.23 no.6
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    • pp.19-23
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    • 2022
  • For the substantiation and verification of studies related to the construction of a levee using riverbed soil, real-scale levee construction and experimental studies are essential. One of the most important factors in the experimental study is the reproducibility of the multiple levees with the same initial conditions. Quantitative analysis of the reproducibility should be presented. In this study, a number of physical properties (specific gravity test, sieving test, liquid-plastic limit test, compaction test, on-site Density test) for multiple embankments built with fine-grained bed soil was obtained. The collected data then used to obtain the possibility of reproducing levee through statistical analysis to suggest a process of indicating a numeric initial condition of the real-scale test. As a result of statistical analysis to verify the aforementioned process, it was confirmed that it was possible to quantitatively evaluate the reproducibility of the construction under the same conditions of embankments. This is expected to be a basic data for a full-scale embankment test using riverbed soil including other soil based real-scale tests.

Aeroelastic Compatibility Substantiation of Aircraft External Stores Using the Dynamic Characteristic Data from Ground Vibration Test (지상진동시험 동특성 데이터를 활용한 항공기 외부장착물의 공력탄성학적 적합성 입증)

  • Lim, Hyun Tae;Kwon, Jae Ryong;Byun, Kwan Hwa;Kim, Hee Joong;Kim, Jae hoon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.45 no.4
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    • pp.269-275
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    • 2017
  • The aeroelastic stability of a fighter type aircraft can be severly affected by the store mass, aerodynamic characteristics, and store combinations. Hence, the stability for the all store configurations must be substantiated before the aircraft in service. For the aeroelastic analysis, the design data and information for the aircraft structure, mass distribution, control surface characteristics, and external shape etc. are required. This is the reason that the store compatibility substantiations by a third party are restricted. However, according to the change of operational environment or the improvement of avionic technology, a new external store is developed and it should be installed on an aircraft without the support from the original supplier. This paper describe the process to substantiate the aeroelastic compatibility between a new external store and an imported aircraft whose design data is not available to a third party operating the aircraft.