참고문헌 (19)

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2. Australian Transport Safety Bureau (ATSB) Technical Analysis Report. Examination of a failed Rolls-Royce RB211-524 Turbofan Engine, Boeing Commercial Aircraft Group, 747-436, G-BNLD; 2002, March. Report No.: 20/02. 

3. United Kingdom Air Accident Investigation Branch (AAIB) Bulletin. Report on the Accident to Dassault-Breguet Mystere-Falcon 900B, G-HMEV; 2007, Jan. Report No.: EW/C2007/01/04. 

4. Society of Automotive Engineers Committee on Engine Containment. Report on Aircraft Engine Containment; 1987, Sept. Report No.: SAE-AIR-4003. 

5. FAA Advisory Circular. Design considerations for minimizing hazards caused by uncontained turbine engine and auxiliary power unit rotor failure. Federal Aviation Administration; 1997, March. Report No.: 20-128A. 

6. Mathis JA. Design and analysis of turbine rotor fragment hazard containment. Federal Aviation Administration; 1997. Report No.: AR-96/121. 

7. Department of Transportation, Federal Aviation Administration. Explicit FEA modeling of multi-layer composite fabric for gas turbine engines containment systems. Final report; 2004, Sept. Report No.: AR-04/40. 

8. McCarthy D. Type of rotor failure and characteristics of fragments. 1997 March. Report No.: NASA CP-2017. 

9. 10.1115/91-GT-163 Dewhurst TB. The impact load on containment rings during a multiple blade shed in aircraft gas turbine engines. International Gas Turbine and Aeroengine Congress and Exposition; 1991; 91-GT-163. 

   

10. ASME International Journal of Materials Engineering and Performance Hebsur 12 4 470 2003 10.1361/105994903770343033 Impact resistance of lightweight hybrid structures for gas turbine engine fan containment applications 

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11. Aerospace Science and Technology Xuan 10 6 501 2006 10.1016/j.ast.2006.04.006 Aeroengine turbine blade containment tests using high-dpeed rotor dpin testing facility 

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12. Finite Elements in Analysis and Design Sarkar 23 2-4 211 1996 10.1016/S0168-874X(96)80008-4 Effects of multiple blade interaction on the containment of blade fragments during a rotor failure 

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13. 10.2514/6.1993-1817 Mathis JA, Parduhn SC, Alvarez P. Analysis of turbine rotor containment and shielding structures. In: AIAA/SAE/ASME/ASEE 29th Joint Propulsion Conference and Exhibit, 1993. Report No. AIAA-93-1817. 

    

14. Carney K, Pereira M, Revilock D, Matheny P. Jet engine fan blade containment using two alternate geometries. The 4th European LS-DYNA conference, 2003; I-I-01-I-I-10. 

15. 10.2514/6.2001-1633 Robert GD, Revilock DM. Impact testing and analysis of composites for aircraft engine fan cases. 2002 April. Report No.: NASA TM-2002-211493. 

    

16. Astrid K, Jorg F. Containment and penetration simulation in case of blade loss in a low pressure turbine. In: DYNA more LS-DYNA Forum, 2002. 

17. International Journal of Impact Engineering Pereira 25 8 715 2002 10.1016/S0734-743X(01)00018-5 Effects of heat treatment on the ballistic impact properties of Inconel 718 for jet engine fan containment applications 

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18. Simons J, Erlich D, Shockey D. Explicit finite element modeling of multilayer composite fabric for gas turbine engine containment systems. Part 3: model development and simulation of experiments. Federal Aviation Administration; 2004. Report No.: AR-04/40/P3. 

19. Department of Transportation, Federal Aviation Administration. Explicit finite element modeling of multilayer composite fabric for gas turbine engine containment systems. Final report; 2009. Report No.: AR-08/37.