journal article·2008-03Open access

Transient three dimensional finite element analysis of a bird striking a fan blade

R. H. Mao, S. A. Meguid, T. Y. Ng

Abstract

A comprehensive three-dimensional nonlinear finite element analyses were carried out to examine the effects of the geometry and the incidence angle of canonical 4-lb bird striking a stationary fan blade using LS-DYNA. Three aspects of the work were accordingly examined. The first was concerned with the modeling framework used. The second with the constitutive law that governs the behaviour of the bird. The third was concerned with the influence of the geometry and the angle of incidence of the bird on the integrity of the blade. This article combines and extends the earlier works on both the Lagrangian modeling methodology (Mao et al. AIAA J. Aircr. 44 (2), 583–596, 2007) and the bird geometry studies (Meguid et al. 2008) in systematic and integrated manner. Both the bird and the blade were simulated in a Lagrangian framework. Furthermore, the homogenized fluidic constitutive equation of the bird follows the Brockman hydrodynamic model, while the blade is modeled as a viscoplastic material of the Perzyna type. The study focused on the three most-frequently used configurations in the literature; namely, hemispherical-ended cylinder, straight-ended cylinder, and ellipsoid, at various length-to-diameter aspect ratios. The results show that the initial contact area between the bird and target in the early phase of the impact event would have a significant effect on the peak impact force. Normal incidence results in maximum impact forces and plastic strains leading to severe deformation. For the case where the incidence angle is equal to or larger than 60°, the impact forces are significantly reduced and the blade deformation remains within the elastic range. The maximum impact force and the resulting plastic strain are not merely governed by the size of the bird but also its density.
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Research context

OpenAlex topics: Fluid Dynamics Simulations and Interactions · Granular flow and fluidized beds · High-Velocity Impact and Material Behavior

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References (35)

Show source-provided references
1. Aiello, R.A., Hirschbein, M.S., Chamis, C.C.: Structural dynamics of shroudless, hollow fan blades with composite in-lays. NASA Tech. Memo. (1982)10.1115/82-GT-284 ↗
2. Airoldi, A., Cacchione, B.: Numerical analyses of bird impact on aircraft structures undergoing large deformations and localized failures. Impact loading of lightweight structures. WIT Trans. Eng. Sci. 49, (2005)
3. Airoldi, A., Cacchione, B.: Modelling of impact forces and pressures in Lagrangian bird strike analyses. Int. J. Impact Eng. 32, 1651–1677 (2006)10.1016/j.ijimpeng.2005.04.011 ↗
4. Alexander, A.: Interactive multi-mode blade impact analysis. ASME Pap. 81-GT-79 (1981)10.1115/81-GT-79 ↗
5. Anghileri, M., Bisagni, C.: Specific problems related to simulation of a bird impact against a turbofan inlet. In Proceeding of the International Crashworthiness Conference 2000 (ICRASH 2000), pp. 652–662. London, UK (2000)
6. Anghileri, M., Luigi, M.L.C., Valerio, M.: Bird strike: approaches to the analysis of impacts with penetration. Impact loading of lightweight structures. WIT Trans. Eng. Sci. 49, 63–74 (2005)
7. Audic, S., Berthillier, M., Bonini, J., Bung, H., Combescure, A.: Prediction of bird impact in hollow fan blades. 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA paper AIAA 2000-3201, Huntsville, Alabama, USA. 16–19 July (2000)10.2514/6.2000-3201 ↗
8. Barber, J.P., Taylor, H.R., Wilbeck, J.S.: Bird impact forces and pressures on rigid and compliant targets. Technical Report AFFDL-TR-77–60. University of Dayton Research Institute, Dayton, OH, USA. (1978)
9. Bowman, D.R.: International birdstrike research group (IBRG) development of a new artificial bird. ASTM F7.08 2004 Transparency Technical Seminar. Washington DC (2004)
10. Brockman, R.A., Held, T.W.: Explicit finite element method for transparency impact analysis. WL-TR-91-3006. University of Dayton Research Institute, Dayton (OH-USA) (1991)
11. Feng, Y.T., Han, K., Owen, D.R.J.: Discrete element simulation of the dynamics of high energy planetary ball milling processes. Mater. Sci. Eng. A Struct. Mater. 375, 815–819 (2004)10.1016/j.msea.2003.10.162 ↗
12. French, R.F.: Test techniques and equipment for the development of air craft engine components resistant to bird ingestion. ASME Pap. 19, 20–26 (1974)
13. Frischbier, J.: Bird strike capability of a transonic fan blisk. Proceedings of the ASME Turboexpo 1997, Orlando, Florida, USA (1997)
14. Gao, D.P., Li, Q.H.: Analytical and experimental investigation of bird impact on blades. J. Aerosp. Power 5(4), 335–338 (1990)
15. Guan, Y.P., Chen, W., Huang, Z.Y.: Sliced model for bird impacting blades. J. Nanjing Univ. Aeronaut. Astronaut. 36(6), 784–786 (2004)
16. Langrand. B., Bayart, A.S., Chauveau, Y., Deletombe, E.: Assessment of multi-physics FE methods for bird strike modeling—application to a metallic riveted airframe. Int. J. Crashworth. 7(4), 415–428 (2002)
17. Lawson, M., Turley, R.: Supercomputer simulation of a birdstrike on a turbofan aero engine. Finite Elem. News 3, 10–14 (1987)
18. Letellier, A., Bung, H., Galon, P., Berthillier, M.: Bird impact on fan blade analysis using smooth particle hydrodynamics coupled with finite elements. ASME Pres. Ves. Pip. Div. 351, 191–195 (1997)
19. Mao, R.H., Meguid, S.A., Ng, T.Y.: Finite element modeling of a bird striking an engine fan blade. AIAA J. Aircr. 44(2), 583–596 (2007)10.2514/1.24568 ↗
20. Martin, N.F.: Nonlinear finite-element analysis to predict fan-blade damage due to soft-body impact. J. Propul. Power 6(4), 445–450 (1990)10.2514/3.25455 ↗
21. McCarthy, M.A., Xiao, J.R., McCarthy, C.T., Kamoulakos, A., Ramos, J., Gallard, J.P., Melito, V.: Modelling of bird strike on an aircraft wing leading edge made from fibre metal laminates—part 2: modeling of impact with SPH bird model. Appl. Compos. Mater. 11, 317–340 (2004)10.1023/B:ACMA.0000037134.93410.c0 ↗
22. Meguid, S.A., Mao, R.H., Ng, T.Y.: FE analysis of geometry Effects of an artificial bird striking an aeroengine fan blade. Int. J. Impact Eng. 35, 487–498 (2008)10.1016/j.ijimpeng.2007.04.008 ↗
23. Miyachi, T., Okumura, H., Ohtake, K.: Analysis of the effect of centrifugal force on the impact resistance of composite fan blades for turbo-fan engines. Proc. Soc. Automot. Eng. 246, 619–626 (1991)
24. Paul, E.: Jet engine certification standards. International Bird Strike Committee ISBC25/WP-IE1, Amsterdam (2000)
25. Perzyna, P.: Fundamental problems in viscoplasticity. Adv. Appl. Mech. 9, 313–377 (1968)
26. Richard, B.: The development of a substitute artificial bird by the international Bird strike Research Group for use in aircraft component testing. International Bird Strike Committee ISBC25/WP-IE3, Amsterdam (2000)
27. Schuette, W.: Blade behavior during bird strike. Science and engineering on supercomputers. Proceedings of the 5th International Conference, pp. 145–157 (1990)
28. Seamans, T.W., Hamershock, D.W., Bernhardt, G.E.: Determination of body density for 12 bird species. IBIS 137(3), 424–428 (1995)10.1111/j.1474-919X.1995.tb08046.x ↗
29. Shimamura, K., Shibue, T., Grosch, D.: Numerical simulation of bird strike damage on jet engine fan blade. ASME Pres. Ves. Pip. Div. 485(1), 161–166 (2004)
30. Shioya, T., Stronge, W.J.: Impact bending of a rotating, rigid-plastic fan blade. J. Propul. Power 1(5), 375–380 (1985)10.2514/3.22812 ↗
31. Stoll, F., Brockman, R.A.: Finite element simulation of high-speed soft-body impacts. Proceedings of the 1997 38th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Part 1, Kissimmee, FL, USA, pp. 334–344 (1997)10.2514/6.1997-1093 ↗
32. Teichman, H.C., Tadros, R.N.: Analytical and experimental simulation on fan blade behavior and damage under bird impact. J. Eng. Gas Turb. Power 113, 582–594 (1991)10.1115/1.2906281 ↗
33. Wilbeck, J.S.: Impact behavior of low strength projectiles. Report No. AFML-TR-77–134, Air Force Materials Lab., Air Force Wright Aeronautical Lab’s, Wright-Patterson Air Force base, OH (1977)
34. Wilbeck, J.S., Rand, J.L.: The development of a substitute bird model. ASME Paper ASME 81-GT-23, Gas turbine conference and products show, Houston TX USA (1981)
35. Willows, M., Driffill, B.: GARTEUR (Group for Aeronautical Research and Technology in EURope) Bird Strike Group, Round robin work package: Rigid wall phase 1 and task 1, DERA Farnborough, Building A7, Room 2008, Hants GU14 OLX (1999)