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    Computational modeling of ice cracking and break-up from helicopter blades

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    Type
    Conference Paper
    Authors
    Shiping, Zhang
    Khurram, Rooh Ul Amin
    Fouladi, Habibollah
    Habashi, Wagdi G (Ed)
    KAUST Department
    KAUST Supercomputing Laboratory (KSL)
    Core Labs
    Date
    2012-09-06
    Online Publication Date
    2012-09-06
    Print Publication Date
    2012-06-25
    Permanent link to this record
    http://hdl.handle.net/10754/564578
    
    Metadata
    Show full item record
    Abstract
    In order to reduce the danger of impact onto components caused by break-up, it is important to analyze the shape of shed ice accumulated during flight. In this paper, we will present a 3D finite element method (FEM) to predict the shed ice shape by using a fluid-solid interaction (FSI) approach to determine the loads, and linear fracture mechanics to track crack propagation. Typical icing scenarios for helicopters are analyzed, and the possibility of ice break-up is investigated.
    Citation
    Shiping, Z., Khurram, R. A., Fouladi, H., & Habashi, W. (2012). Computational Modeling of Ice Cracking and Break-up from Helicopter Blades. 4th AIAA Atmospheric and Space Environments Conference. doi:10.2514/6.2012-2675
    Publisher
    American Institute of Aeronautics and Astronautics (AIAA)
    Journal
    4th AIAA Atmospheric and Space Environments Conference
    Conference/Event name
    4th AIAA Atmospheric and Space Environments Conference 2012
    ISBN
    9781624101922
    DOI
    10.2514/6.2012-2675
    ae974a485f413a2113503eed53cd6c53
    10.2514/6.2012-2675
    Scopus Count
    Collections
    Conference Papers; KAUST Supercomputing Laboratory (KSL)

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