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http://dx.doi.org/10.20910/JASE.2019.13.6.70

Study on Verification Methodology of Airworthiness Requirements for Bird Strike on Civilian Helicopter based on Numerical Analysis  

Kim, Dong-Hyeop (Department of Mechanical Engineering, Hankyong National University)
Kim, Sang-Woo (Department of Mechanical Engineering, Hankyong National University)
Kim, Hyun-Gi (Aeronautics Research and Development Head Office, Korea Aerospace Research Institute)
Kim, Sungchan (Aeronautics Research and Development Head Office, Korea Aerospace Research Institute)
Shin, Bok Kyun (Strategic Planning Office, Korea Aerospace Industries Association)
Publication Information
Journal of Aerospace System Engineering / v.13, no.6, 2019 , pp. 70-79 More about this Journal
Abstract
The increase of bird strike requires to be amended more safely current airworthiness requirements for bird strike. The USA and Europe are considering the methodology to verify the bird strike requirements based on the finite element analysis (FEA). Meanwhile, the aircraft airworthiness standards in Korea enacted by the Ministry of Land, Infrastructure and Transport were based on those enacted by the Federal Aviation Administration (FAA). This means that the verification methods using the FEA for the bird strike requirements should be reflected in the airworthiness standards in Korea. Our study proposes the methodology for bird strike simulation based on the FEA for the external auxiliary fuel tank assembly on the Surion helicopters and confirmed that the numerical outputs corresponded to the test results. The authors suggest that the methodology and procedure based on the FEA are adopted not only in the bird strike requirements but in various aircraft certifications of civilian rotorcraft.
Keywords
Aircraft Certification; Bird Strike; Helicopter; Finite Element Analysis; External Auxiliary Fuel Tank Assembly;
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Times Cited By KSCI : 1  (Citation Analysis)
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1 Ministry of Land, Infrastructure, and Transport, "Reports of bird strike accident 2010-2016," Sejong City, Republic of Korea, May 2016
2 R. A. Dolbeer, S. E. Wright, J. Weller, and M. J. Begier, "Wildlife strikes to civil aircraft in the United States 1990-2013," FAA Technical report, Office of Airport Safety and Standards, Washingtion D.C., Jan. 2014.
3 F. Faith, "Miracle on the Hudson' passenger to speak on Feb. 20," The Tullahoma News (https://tullahomanews.com/), Feb. 2019.
4 S. M. Lee, J. K. Hwang, and Y. K. Kim, "Bird strike requirements for helicopter and substantiation of Surion windshield," Proc. of Conf. The Korean Society for Aeronautical and Space Sciences, Jeju-do, Republic of Korea, pp. 484-485, Nov. 2017.
5 M. L. Ugone, J. E. Meling, J. D Snider, N. J. Gause, and A. F. Carrey, "Acquisition: Fuel cells of the V-22 Osprey joint advanced vertical aircraft," Inspector General of the Department of Defense, Arlington, Oct. 2002.
6 M. Guida, F. Marulo, M. Meo, A. Grimaldi, and G. Olivares, "SPH-Lagrangian study of bird impact on leading edge wing," Composites Structures, vol. 93, no. 3, pp. 1060-1071, Feb. 2011.   DOI
7 K. Y. Lee, B. J. Yi, H. G. Chung, and C. K. Ryoo, "A study on certification procedures for aircraft parts manufacturer approval," Journal of The Korean Society for Aeronautical and Space Sciences, vol. 42, no. 12, pp. 1073-1079, Dec. 2014.   DOI
8 D. H. Kim and S. W. Kim, "Numerical investigation of impact-induced damage of auxiliary composite fuel tanks on Korean Utility Helicopter," Composites, Part B: Engineering, vol. 165, pp. 301-311, May 2019.   DOI
9 D. H. Kim and S. W. Kim, "Evaluation of bird strike-induced damages of helicopter composite fuel tank assembly based on fluid-structure interaction analysis," Composite Structures, vol. 210, pp. 676-686, Feb. 2019.   DOI
10 D. J. Benson, "Computational methods in Lagrangian and Eulerian hydrocodes," Computer Methods in Applied Mechanics and Engineering, vol. 99, no. 2-3, pp. 235-394, Sep. 1992.   DOI
11 J. H. Jo and Y. S. Lee, "Quantitative analysis of de bris clouds of aluminum plates with SPH," Proc. of Conf. The Society of CAD/CAM, Pyeongchang-gun, Republic of Korea, pp. 755-760, Jan. 2013.
12 R. A. Gingold and J. J. Monaghen, "Smoothed particle hydrodynamics: theory and application to non-spherical stars," Monthly Notices of The Royal Astronomical Society, vol. 181, no. 3, pp. 375-389, Dec. 1977.   DOI
13 X. Yang, Z. Zhang, J. Yang, and Y. Sun, "Fluid-structure interaction analysis of the drop impact test for helicopter fuel tank," Springerplus, vol. 5, no. 1, pp. 1573, Dec. 2016.   DOI
14 Dassault, "Abaqus Analysis User's manual - Section 15.2.1," Abaqus 6.13 edition, Apr. 2013.
15 Z. Hashin, "Failure criteria for unidirectional fiber composites," Journal of Applied Mechanics, vol. 47, pp. 329-334, Jun. 1980.   DOI
16 Z. Hashin and A. Rotem, "A fatigue failure criterion for fiber-reinforced materials," Journal of Composite Materials, vol. 7, pp. 448-464, Oct. 1973.   DOI
17 M. Y. Park, Y. J. Kim, J. H. Kim, S. Y. Jang, and C. Y. Park, "Bird strike test and result analysis for the safety design of aircraft structures," Proc. of Conf. The Korean Society for Aeronautical and Space Sciences, Wonju-si, Republic of Korea, pp. 293-296, Apr. 2010.
18 J. S. Wilbeck, "AFMLTR-77-134: Impact behaviour of low-strength projectiles," Technical report Air Force Materials Laboratory, Wright-Patterson Air Force Base, State of Ohio, Jul. 1978.
19 N. Nanami and O. O. Ochoa, "Damage assessment of a large-scale hybrid composite wind turbine blade," Journal of Mechanical Engineering and Automation, vol. 6, no. 5, pp. 117-127, 2016.
20 H. G. Kim and S. C. Kim, "A numerical study on the influence of the amount of internal fuel in a bird strike test for the external auxiliary fuel tank of rotorcraft," International Journal of Crashworthiness, pp. 1-15, Dec. 2017.
21 P. Kumar and B. Rai, "Delaminations of barely visible impact damage in CFRP laminates," Composite Structures, vol. 23, pp. 313-318, 1993.   DOI