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An Extensive Crashworthiness Methodology for Advanced Propulsion Systems, Part I: Soft Impact Damage Assessment of Composite Fan Stage Assemblies
Abstract
Jet engines are the most susceptible aircraft structures to catastrophic damage caused by soft impact events, such as ingesting birds or hail stones. Future propulsion systems will incorporate advanced composites, particularly in the fan assembly, because of their superior strength and stiffness properties compared to metals. However, reliance on physical testing to assess the crashworthiness of engine designs currently inhibits the development of novel propulsion concepts. The findings presented in this work are part of a study aimed at developing an extensive analytical methodology for predicting and assessing damage to engine forward sections containing composite structures. In this study, a modeling approach for capturing damage due to bird strike on composite fan blades and a fan assembly was developed. Impacts on a pre-stressed composite static single blade and a full rotating fan assembly were simulated. Two numerical methods were used to model the bird using an explicit finite element (FE) code: (1) an arbitrary Lagrangian-Eulerian (ALE) method, and (2) a meshless Lagrangian particle method. First, these models were calibrated, generating interface impact pressure results that correlated well with experimental data and previous extensive FE results. Next, bird strike simulations on a single blade were carried out, with each approach capable of producing damage and failure within the composite structure. Finally, an impact scenario on a full fan stage rotating at 7200…
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Research works printed but not linked: 46
- Yupu G., 2007, ChineseJournal ofAeronautics., 20, 408
- Teichman H.C., 1991, Journal ofengineeringfor gasturbinesandpower, 113, 582
- Vasko T.J., 2000, Proceedings of 6th International LS-DYNA Users Conference
- 10.2514/3.25455 · DOI
- 10.2514/3.45002 · DOI
- Shultz C., Peters. J., 2002
- Meguid S.A., 2008, International JournalofImpact Engineering, 34, 487, 10.1016/j.ijimpeng.2007.04.008 · DOI · Paper page
- 10.2514/1.24568 · DOI
- Ryabov A.A., 2007, Proceedingsof6thEuropean LS-DYNAUser'sConference
- 10.1007/s10999-008-9067-1 · DOI
- Chamis C.C., Technical Papers on Structuresand Materials, 1979, 249
- Menouillard T., 2006, Proceedings of Journal De Physique. IV, 134, 409
- 10.2514/3.58354 · DOI
- 10.1115/PVP2004-2867 · DOI
- Jenq S.T., Computational Materials Science, 2006, 1
- Lagrand B., 2002, International Journal of Crashworthiness, 7, 415
- 10.1007/BF02484547 · DOI
- Yupu G., 2008, ChineseJournalofAeronautics, 21, 328
- 10.1115/PVP2004-2870 · DOI
- Frischbier J., 2007, AIAA, 2005
- 10.1016/S1000-9361(07)60075-2 · DOI
- McCallum S.C., 2005, Proceedings of the 5th European LS-DYNAUsersConference
- Hanssen A.G., 2006, International JournalofImpact Engineering, 32, 1127, 10.1016/j.ijimpeng.2004.09.004 · DOI
- Wilbeck J.S., 1975, AFFDL-TR-, 75, A021142
- Georgiadis S., 2008, CompositeStructures, 86, 258
- Anghileri M., 2005, Proceedingsof5th European LS-DYNAUsersConference
- Joosten M., 2006, Impact damage modelling of composite aerospace structures subject tobird-strike
- 10.1115/1.2906207 · DOI
- 31Cheng, J., Biniend, W.K. "Simulation of Soft Projectiles Impacting Composite Targets using an Arbitrary Lagrangian-Eulerian Formulation"Journal ofaircraft Vol43,No.6,2006, pp,1726-1731 · DOI
- Hassen A., 2006, International JournalofImpact Engineering, 32, 1127, 10.1016/j.ijimpeng.2004.09.004 · DOI
- Hormann M., 2004, Horizontal tailplanesubjected to impact loading,"Proceedings of8th International LS-DynaUsersConference
- Anghileri M., 2005, WIT Transactionson EngineeringSciences, 49, 63
- Airoldi A., 2006, International JournalofImpact Engineering, 32, 1651, 10.1016/j.ijimpeng.2005.04.011 · DOI
- Iannucci L., IMechEseminarpublication, 1998, 11
- 10.1016/S0263-8223(03)00033-3 · DOI
- Barber J.P., 1977, Bird Impact Forces and Pressures on Rigid and Compliant Targets
- Thomson D., 1994, AIAA, 369
- Carney K.S., 2002, Proceedings of 7th International LSDYNAUsersConference
- 10.1115/1.3269873 · DOI
- Wilbeck, 1978, TheShockandVibrationBulletin, 48, 115
- Tata D., 2006, School of Aerospace Mechanical and ManufacturingEngineering.
- Zammit A., 2008, Proceedingsof26thInternationalCongressoftheAeronauticalSciences
- Hallquist J.O., 2006, LS-DYNATheoryManual
- 2007, LS-DYNA Keyword User‟s Manual, 1
- Schwizerho K., Crashworthiness Analysis with Enhanced Composite Material Models in LS-DYNA-Meritsand Limits,"Proceedingsof 5thInternational LS-DYNAUser‟sConference,1998
- 10.2514/6.2011-981 · DOI
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Soft impacts on aerospace structures
Abrate, S. (2016) · Progress in Aerospace Sciences · doi:10.1016/j.paerosci.2015.11.005 · Cited by 84
Impact responses of slender composite plates for bird-strike testing of fan blades
Zhou, Y., Sun, Y., & Huang, T. (2019) · Latin American Journal of Solids and Structures · doi:10.1590/1679-78255809 · Cited by 24
“Future propulsion systems will incorporate advanced composites, particularly in the fan assembly, because of their superior strength and stiffness properties compared to metals (Kim et al., 2011).”
Background
Metadata
- Authors
- Kim, M., Zammit, A., Siddens, A., & Bayandor, J.
- Affiliations
- School of Aerospace, Mechanics & Manufacturing Engineering
- Dpeartment of Mechanical Engineering
- Department of Mechanical Engineering
- Venue
- 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
- Published
- 2011-01-04
- OpenAlex
- W2321229301
- Cited by
- 13
- References
- 0
- Citations by year
- 2022: 1 · 2021: 2 · 2020: 1 · 2019: 2 · 2018: 1 · 2015: 1 · 2014: 1 · 2013: 2 · 2012: 1
- FWCI
- 7.24
- Type
- conference paper
- Language
- en
- Open access
- closed
- Locations
- AIAA Aerospace Sciences Meeting (publishedVersion)
- Topics
- Physical Sciences › Engineering › Mechanics of Materials › Mechanical Behavior of Composites
- Physical Sciences › Engineering › Mechanics of Materials › High-Velocity Impact and Material Behavior
- Physical Sciences › Engineering › Automotive Engineering › Transportation Safety and Impact Analysis
- Keywords
- crashworthiness, bird strikes, composite fan blades, arbitrary Lagrangian-Eulerian method, impact pressure
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