Safety and Accidents Involving Aircraft Manufactured from Polymer Composite Materials: A Review
Abstract The aviation accident investigation process includes the detailed examination of the aircraft wreckage, as well as the analysis of both primary and secondary elements of the aircraft structure. This requires examination of the wreckage at the accident site, and is followed by additional ana...
Ausführliche Beschreibung
Autor*in: |
Di Giorgio, Giovanni [verfasserIn] |
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E-Artikel |
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Sprache: |
Englisch |
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2023 |
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Anmerkung: |
© The Author(s) under exclusive licence to AIDAA Associazione Italiana di Aeronautica e Astronautica 2023. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. |
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Übergeordnetes Werk: |
Enthalten in: Aerotecnica missili & spazio - [Cham] : Springer International Publishing, 2001, 102(2023), 4 vom: 30. Aug., Seite 337-353 |
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Übergeordnetes Werk: |
volume:102 ; year:2023 ; number:4 ; day:30 ; month:08 ; pages:337-353 |
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DOI / URN: |
10.1007/s42496-023-00170-9 |
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Katalog-ID: |
SPR053756568 |
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10.1007/s42496-023-00170-9 doi (DE-627)SPR053756568 (SPR)s42496-023-00170-9-e DE-627 ger DE-627 rakwb eng Di Giorgio, Giovanni verfasserin (orcid)0009-0007-5293-2458 aut Safety and Accidents Involving Aircraft Manufactured from Polymer Composite Materials: A Review 2023 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s) under exclusive licence to AIDAA Associazione Italiana di Aeronautica e Astronautica 2023. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. Abstract The aviation accident investigation process includes the detailed examination of the aircraft wreckage, as well as the analysis of both primary and secondary elements of the aircraft structure. This requires examination of the wreckage at the accident site, and is followed by additional analysis, often driven by the first results on the field. Therefore, one of the most important tasks of investigators is to determine the sequence of events of the accident. This means that much evidence should be collected to accurately determine the order in which events occurred. With regard to construction materials involved, the interpretation of fracture surfaces can provide very important information. However, metallic and composite structures demonstrate very different behaviors during the operative service, from corrosion and fatigue to fire and combustion resistance. This paper performs a literature review on the identification of failure mode, damage and safety of polymer composite aircraft structures from a point of view that may be useful to aviation safety investigations, with the aim to provide suggestions for future research. Aircraft (dpeaa)DE-He213 Accident (dpeaa)DE-He213 Polymer (dpeaa)DE-He213 Composite (dpeaa)DE-He213 Failure (dpeaa)DE-He213 Fracture (dpeaa)DE-He213 Fire (dpeaa)DE-He213 Enthalten in Aerotecnica missili & spazio [Cham] : Springer International Publishing, 2001 102(2023), 4 vom: 30. Aug., Seite 337-353 (DE-627)1047764040 (DE-600)2960384-5 2524-6968 nnns volume:102 year:2023 number:4 day:30 month:08 pages:337-353 https://dx.doi.org/10.1007/s42496-023-00170-9 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 102 2023 4 30 08 337-353 |
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10.1007/s42496-023-00170-9 doi (DE-627)SPR053756568 (SPR)s42496-023-00170-9-e DE-627 ger DE-627 rakwb eng Di Giorgio, Giovanni verfasserin (orcid)0009-0007-5293-2458 aut Safety and Accidents Involving Aircraft Manufactured from Polymer Composite Materials: A Review 2023 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s) under exclusive licence to AIDAA Associazione Italiana di Aeronautica e Astronautica 2023. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. Abstract The aviation accident investigation process includes the detailed examination of the aircraft wreckage, as well as the analysis of both primary and secondary elements of the aircraft structure. This requires examination of the wreckage at the accident site, and is followed by additional analysis, often driven by the first results on the field. Therefore, one of the most important tasks of investigators is to determine the sequence of events of the accident. This means that much evidence should be collected to accurately determine the order in which events occurred. With regard to construction materials involved, the interpretation of fracture surfaces can provide very important information. However, metallic and composite structures demonstrate very different behaviors during the operative service, from corrosion and fatigue to fire and combustion resistance. This paper performs a literature review on the identification of failure mode, damage and safety of polymer composite aircraft structures from a point of view that may be useful to aviation safety investigations, with the aim to provide suggestions for future research. Aircraft (dpeaa)DE-He213 Accident (dpeaa)DE-He213 Polymer (dpeaa)DE-He213 Composite (dpeaa)DE-He213 Failure (dpeaa)DE-He213 Fracture (dpeaa)DE-He213 Fire (dpeaa)DE-He213 Enthalten in Aerotecnica missili & spazio [Cham] : Springer International Publishing, 2001 102(2023), 4 vom: 30. Aug., Seite 337-353 (DE-627)1047764040 (DE-600)2960384-5 2524-6968 nnns volume:102 year:2023 number:4 day:30 month:08 pages:337-353 https://dx.doi.org/10.1007/s42496-023-00170-9 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 102 2023 4 30 08 337-353 |
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10.1007/s42496-023-00170-9 doi (DE-627)SPR053756568 (SPR)s42496-023-00170-9-e DE-627 ger DE-627 rakwb eng Di Giorgio, Giovanni verfasserin (orcid)0009-0007-5293-2458 aut Safety and Accidents Involving Aircraft Manufactured from Polymer Composite Materials: A Review 2023 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s) under exclusive licence to AIDAA Associazione Italiana di Aeronautica e Astronautica 2023. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. Abstract The aviation accident investigation process includes the detailed examination of the aircraft wreckage, as well as the analysis of both primary and secondary elements of the aircraft structure. This requires examination of the wreckage at the accident site, and is followed by additional analysis, often driven by the first results on the field. Therefore, one of the most important tasks of investigators is to determine the sequence of events of the accident. This means that much evidence should be collected to accurately determine the order in which events occurred. With regard to construction materials involved, the interpretation of fracture surfaces can provide very important information. However, metallic and composite structures demonstrate very different behaviors during the operative service, from corrosion and fatigue to fire and combustion resistance. This paper performs a literature review on the identification of failure mode, damage and safety of polymer composite aircraft structures from a point of view that may be useful to aviation safety investigations, with the aim to provide suggestions for future research. Aircraft (dpeaa)DE-He213 Accident (dpeaa)DE-He213 Polymer (dpeaa)DE-He213 Composite (dpeaa)DE-He213 Failure (dpeaa)DE-He213 Fracture (dpeaa)DE-He213 Fire (dpeaa)DE-He213 Enthalten in Aerotecnica missili & spazio [Cham] : Springer International Publishing, 2001 102(2023), 4 vom: 30. Aug., Seite 337-353 (DE-627)1047764040 (DE-600)2960384-5 2524-6968 nnns volume:102 year:2023 number:4 day:30 month:08 pages:337-353 https://dx.doi.org/10.1007/s42496-023-00170-9 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 102 2023 4 30 08 337-353 |
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10.1007/s42496-023-00170-9 doi (DE-627)SPR053756568 (SPR)s42496-023-00170-9-e DE-627 ger DE-627 rakwb eng Di Giorgio, Giovanni verfasserin (orcid)0009-0007-5293-2458 aut Safety and Accidents Involving Aircraft Manufactured from Polymer Composite Materials: A Review 2023 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s) under exclusive licence to AIDAA Associazione Italiana di Aeronautica e Astronautica 2023. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. Abstract The aviation accident investigation process includes the detailed examination of the aircraft wreckage, as well as the analysis of both primary and secondary elements of the aircraft structure. This requires examination of the wreckage at the accident site, and is followed by additional analysis, often driven by the first results on the field. Therefore, one of the most important tasks of investigators is to determine the sequence of events of the accident. This means that much evidence should be collected to accurately determine the order in which events occurred. With regard to construction materials involved, the interpretation of fracture surfaces can provide very important information. However, metallic and composite structures demonstrate very different behaviors during the operative service, from corrosion and fatigue to fire and combustion resistance. This paper performs a literature review on the identification of failure mode, damage and safety of polymer composite aircraft structures from a point of view that may be useful to aviation safety investigations, with the aim to provide suggestions for future research. Aircraft (dpeaa)DE-He213 Accident (dpeaa)DE-He213 Polymer (dpeaa)DE-He213 Composite (dpeaa)DE-He213 Failure (dpeaa)DE-He213 Fracture (dpeaa)DE-He213 Fire (dpeaa)DE-He213 Enthalten in Aerotecnica missili & spazio [Cham] : Springer International Publishing, 2001 102(2023), 4 vom: 30. Aug., Seite 337-353 (DE-627)1047764040 (DE-600)2960384-5 2524-6968 nnns volume:102 year:2023 number:4 day:30 month:08 pages:337-353 https://dx.doi.org/10.1007/s42496-023-00170-9 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 102 2023 4 30 08 337-353 |
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10.1007/s42496-023-00170-9 doi (DE-627)SPR053756568 (SPR)s42496-023-00170-9-e DE-627 ger DE-627 rakwb eng Di Giorgio, Giovanni verfasserin (orcid)0009-0007-5293-2458 aut Safety and Accidents Involving Aircraft Manufactured from Polymer Composite Materials: A Review 2023 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s) under exclusive licence to AIDAA Associazione Italiana di Aeronautica e Astronautica 2023. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. Abstract The aviation accident investigation process includes the detailed examination of the aircraft wreckage, as well as the analysis of both primary and secondary elements of the aircraft structure. This requires examination of the wreckage at the accident site, and is followed by additional analysis, often driven by the first results on the field. Therefore, one of the most important tasks of investigators is to determine the sequence of events of the accident. This means that much evidence should be collected to accurately determine the order in which events occurred. With regard to construction materials involved, the interpretation of fracture surfaces can provide very important information. However, metallic and composite structures demonstrate very different behaviors during the operative service, from corrosion and fatigue to fire and combustion resistance. This paper performs a literature review on the identification of failure mode, damage and safety of polymer composite aircraft structures from a point of view that may be useful to aviation safety investigations, with the aim to provide suggestions for future research. Aircraft (dpeaa)DE-He213 Accident (dpeaa)DE-He213 Polymer (dpeaa)DE-He213 Composite (dpeaa)DE-He213 Failure (dpeaa)DE-He213 Fracture (dpeaa)DE-He213 Fire (dpeaa)DE-He213 Enthalten in Aerotecnica missili & spazio [Cham] : Springer International Publishing, 2001 102(2023), 4 vom: 30. Aug., Seite 337-353 (DE-627)1047764040 (DE-600)2960384-5 2524-6968 nnns volume:102 year:2023 number:4 day:30 month:08 pages:337-353 https://dx.doi.org/10.1007/s42496-023-00170-9 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 102 2023 4 30 08 337-353 |
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safety and accidents involving aircraft manufactured from polymer composite materials: a review |
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Safety and Accidents Involving Aircraft Manufactured from Polymer Composite Materials: A Review |
abstract |
Abstract The aviation accident investigation process includes the detailed examination of the aircraft wreckage, as well as the analysis of both primary and secondary elements of the aircraft structure. This requires examination of the wreckage at the accident site, and is followed by additional analysis, often driven by the first results on the field. Therefore, one of the most important tasks of investigators is to determine the sequence of events of the accident. This means that much evidence should be collected to accurately determine the order in which events occurred. With regard to construction materials involved, the interpretation of fracture surfaces can provide very important information. However, metallic and composite structures demonstrate very different behaviors during the operative service, from corrosion and fatigue to fire and combustion resistance. This paper performs a literature review on the identification of failure mode, damage and safety of polymer composite aircraft structures from a point of view that may be useful to aviation safety investigations, with the aim to provide suggestions for future research. © The Author(s) under exclusive licence to AIDAA Associazione Italiana di Aeronautica e Astronautica 2023. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. |
abstractGer |
Abstract The aviation accident investigation process includes the detailed examination of the aircraft wreckage, as well as the analysis of both primary and secondary elements of the aircraft structure. This requires examination of the wreckage at the accident site, and is followed by additional analysis, often driven by the first results on the field. Therefore, one of the most important tasks of investigators is to determine the sequence of events of the accident. This means that much evidence should be collected to accurately determine the order in which events occurred. With regard to construction materials involved, the interpretation of fracture surfaces can provide very important information. However, metallic and composite structures demonstrate very different behaviors during the operative service, from corrosion and fatigue to fire and combustion resistance. This paper performs a literature review on the identification of failure mode, damage and safety of polymer composite aircraft structures from a point of view that may be useful to aviation safety investigations, with the aim to provide suggestions for future research. © The Author(s) under exclusive licence to AIDAA Associazione Italiana di Aeronautica e Astronautica 2023. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. |
abstract_unstemmed |
Abstract The aviation accident investigation process includes the detailed examination of the aircraft wreckage, as well as the analysis of both primary and secondary elements of the aircraft structure. This requires examination of the wreckage at the accident site, and is followed by additional analysis, often driven by the first results on the field. Therefore, one of the most important tasks of investigators is to determine the sequence of events of the accident. This means that much evidence should be collected to accurately determine the order in which events occurred. With regard to construction materials involved, the interpretation of fracture surfaces can provide very important information. However, metallic and composite structures demonstrate very different behaviors during the operative service, from corrosion and fatigue to fire and combustion resistance. This paper performs a literature review on the identification of failure mode, damage and safety of polymer composite aircraft structures from a point of view that may be useful to aviation safety investigations, with the aim to provide suggestions for future research. © The Author(s) under exclusive licence to AIDAA Associazione Italiana di Aeronautica e Astronautica 2023. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. |
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title_short |
Safety and Accidents Involving Aircraft Manufactured from Polymer Composite Materials: A Review |
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https://dx.doi.org/10.1007/s42496-023-00170-9 |
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