참고문헌 (22)

1. Federal Aviation Administration (United States) 1984 Federal aviation regulation part 33, section 33.94-blade containment and rotor unbalance tests 

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8. Shmotin 2006 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit Numerical analysis of aircraft engine fan blade-out 

9. Heidari 2008 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference An efficient multi-disciplinary simulation of engine fan-blade out event using MD Nastran 

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11. Jain 2010 Proceedings of the IMPLAST 2010 Conference Prediction of transient loads and perforation of engine casing during blade-off event of fan rotor assembly 

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14. Probl. Strength Plast. Ryabov 77 2 172 2015 10.32326/1814-9146-2015-77-2-172-181 Numerical-experimental investigation of turbine engine casing dynamic deformation in blade out 

    

15. J. Zhejiang Univ. Sci. A He 13 4 239 2012 10.1631/jzus.A1100294 Simulation methodology development for rotating blade containment analysis 

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21. J. Mater. Sci. Abotula 46 14 4971 2011 10.1007/s10853-011-5414-y Dynamic constitutive behavior of Hastelloy X under thermo-mechanical loads 

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22. Int. J. Impact Eng. Chennamsetty 85 97 2015 10.1016/j.ijimpeng.2015.06.016 Dynamic response of Hastelloy® X plates under oblique shocks: experimental and numerical studies 

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