Ballistic Penetration Test and Simulation of Metallic Aircraft Wing Fuel Tank
The development of a fighter aircraft requires reasonable assessment and validation of airframe survivability against weapon threats. Fulfilling this objective and effectively meeting the combat survivability requirements necessitates enhanced design based on simulated battle damage and organized li...
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| Published in | International journal of aeronautical and space sciences Vol. 24; no. 1; pp. 303 - 314 |
|---|---|
| Main Authors | , , , |
| Format | Journal Article |
| Language | English |
| Published |
Seoul
The Korean Society for Aeronautical & Space Sciences (KSAS)
01.02.2023
한국항공우주학회 |
| Subjects | |
| Online Access | Get full text |
| ISSN | 2093-274X 2093-2480 |
| DOI | 10.1007/s42405-022-00565-1 |
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| Abstract | The development of a fighter aircraft requires reasonable assessment and validation of airframe survivability against weapon threats. Fulfilling this objective and effectively meeting the combat survivability requirements necessitates enhanced design based on simulated battle damage and organized live fire tests. The hydrodynamic ram effect occurs when a projectile penetrates the wing fuel tank of an aircraft and is the largest single source of aircraft losses. In this study, battle damage prediction and assessment of an aircraft wing fuel tank subjected to the penetration of a ballistic projectile were therefore undertaken using a two-stage live fire test and corresponding simulations. The correlation between test and simulation results was confirmed, thereby establishing techniques for testing and simulating the hydrodynamic ram effect on the aircraft sub-assembly level. |
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| AbstractList | The development of a fighter aircraft requires reasonable assessment and validation of airframe survivability against weapon threats. Fulfilling this objective and effectively meeting the combat survivability requirements necessitates enhanced design based on simulated battle damage and organized live fire tests. The hydrodynamic ram effect occurs when a projectile penetrates the wing fuel tank of an aircraft and is the largest single source of aircraft losses. In this study, battle damage prediction and assessment of an aircraft wing fuel tank subjected to the penetration of a ballistic projectile were therefore undertaken using a two-stage live fire test and corresponding simulations. The correlation between test and simulation results was confirmed, thereby establishing techniques for testing and simulating the hydrodynamic ram effect on the aircraft sub-assembly level. The development of a fighter aircraft requires reasonable assessment and validation of airframe survivability against weapon threats. Fulfilling this objective and effectively meeting the combat survivability requirements necessitates enhanced design based on simulated battle damage and organized live fire tests. The hydrodynamic ram effect occurs when a projectile penetrates the wing fuel tank of an aircraft and is the largest single source of aircraft losses. In this study, battle damage prediction and assessment of an aircraft wing fuel tank subjected to the penetration of a ballistic projectile were therefore undertaken using a two-stage live fire test and corresponding simulations. The correlation between test and simulation results was confirmed, thereby establishing techniques for testing and simulating the hydrodynamic ram effect on the aircraft sub-assembly level. KCI Citation Count: 0 |
| Author | Choi, Kisub Seo, Bohwi Kim, Jong Heon Sung, Siyul |
| Author_xml | – sequence: 1 givenname: Jong Heon orcidid: 0000-0001-9629-4733 surname: Kim fullname: Kim, Jong Heon email: ian0328@add.re.kr organization: Aerospace Technology Research Institute-1, Agency for Defense Development – sequence: 2 givenname: Bohwi surname: Seo fullname: Seo, Bohwi organization: Aerospace Technology Research Institute-1, Agency for Defense Development – sequence: 3 givenname: Kisub surname: Choi fullname: Choi, Kisub organization: Innoqual Co., Ltd – sequence: 4 givenname: Siyul surname: Sung fullname: Sung, Siyul organization: Innoqual Co., Ltd |
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| Cites_doi | 10.1016/j.compstruct.2013.11.022 10.2514/6.2008-1965 10.1016/0013-7944(85)90052-9 10.3390/ma11060938 10.4028/www.scientific.net/AMM.566.457 10.2514/6.2005-2330 10.2514/1.J051613 10.1016/j.procir.2015.04.093 10.1016/j.compstruct.2012.09.020 10.1007/978-3-030-59947-8 10.2514/6.2005-7647 |
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| Copyright | The Author(s), under exclusive licence to The Korean Society for Aeronautical & Space Sciences 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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| Keywords | Ballistic penetration Battle damage Structural vulnerability and survivability Hydrodynamic ram Aircraft fuel tank |
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| References | Chagas G, Machado I (2015), Numerical model of machining considering the effect of MnS inclusions in an austenitic stainless steel. 15th CIRP conference on modelling of machining operations, pp 533–538 HouXLiuZWangBLvWLiangXHuaYStress-strain curves and modified material constitutive model for Ti-6Al-4V over the wide ranges of strain rate and temperatureMaterials201810.3390/ma11060938 TuckerJNext generation fire modeling, aircraft survivability2017BerlinSpring713 Artero-GuerreroJAPernas-SanchezJVarasDLopez-PuenteJNumerical analysis of CFRP fluid-filled tubes subjected to high-velocity impactCompos Struct20139628629710.1016/j.compstruct.2012.09.020 Hinrichsen R, Stratton S, Moussa A, Zhang G (2008) Hydrodynamic ram simulator. Joint aircraft survivability program report, JASPO-V-07-06-001, Wright-Patterson, OH Czarnecki G, Maxson M, Sawdy J, Miller M, Hinrichsen R (2006) Evaluation of skin spar joint resistance to hydrodynamic ram. Air force material command public affairs office, AFRLWS-WP-TR-2007-9002 VarasDLopez-PuenteJZaeraRNumerical analysis of the hydrodynamic ram phenomenon in aircraft fuel tanksAIAA20125071621163010.2514/1.J051613 Lamberson L, Mates S, Eliasson V (2020) Dynamic behavior of materials. Proceedings of the 2020 annual conference on experimental and applied mechanics, vol 1 Gonzalez M, Sparks C, Kubes C, Girard W (2008) Comparison of the tumbling behavior and pressure evolution of several API projectiles in a hydrodynamic ram environment. 49th AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials conference, Schaumburg AIAA 2008-1965:1-15. https://doi.org/10.2514/6.2008-1965 HeimbsSNogueiraAHombergsmeierEMayMWolfrumJFailure behavior of composite T-joints with novel metallic arrow-pin reinforcementCompos Struct2014110162810.1016/j.compstruct.2013.11.022 Moussa NA, Whale MD, Groszmann DE, Zhang XJ (1997) The potential for fuel tank fire and hydrodynamic ram from uncontained aircraft engine debris. DOT/FAA/AR-96/95, BlazeTech corporation, Cambridge, MA Weisenabach M, Kurtz A, Czarnecki G (2005) Update on the joint aircraft survivability. 49th AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials conference, Austin, Texas AIAA 2005-2330:1–4. https://doi.org/10.2514/6.2005-2330 JohnsonGCookWFracture characteristics of three metals subjected to various strains, strain rates, temperatures and pressuresEng Fract Mech1985211314810.1016/0013-7944(85)90052-9 Flores-JohnsonEShenLNguyenGFinite-element modelling of the impact behaviour of aluminum nacre-like compositeAppl Mech Mater201410.4028/www.scientific.net/AMM.566.457 565_CR12 565_CR10 D Varas (565_CR6) 2012; 50 565_CR13 565_CR1 X Hou (565_CR11) 2018 S Heimbs (565_CR5) 2014; 110 JA Artero-Guerrero (565_CR7) 2013; 96 G Johnson (565_CR8) 1985; 21 J Tucker (565_CR14) 2017 E Flores-Johnson (565_CR9) 2014 565_CR4 565_CR3 565_CR2 |
| References_xml | – reference: Chagas G, Machado I (2015), Numerical model of machining considering the effect of MnS inclusions in an austenitic stainless steel. 15th CIRP conference on modelling of machining operations, pp 533–538 – reference: HouXLiuZWangBLvWLiangXHuaYStress-strain curves and modified material constitutive model for Ti-6Al-4V over the wide ranges of strain rate and temperatureMaterials201810.3390/ma11060938 – reference: Weisenabach M, Kurtz A, Czarnecki G (2005) Update on the joint aircraft survivability. 49th AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials conference, Austin, Texas AIAA 2005-2330:1–4. https://doi.org/10.2514/6.2005-2330 – reference: Czarnecki G, Maxson M, Sawdy J, Miller M, Hinrichsen R (2006) Evaluation of skin spar joint resistance to hydrodynamic ram. Air force material command public affairs office, AFRLWS-WP-TR-2007-9002 – reference: HeimbsSNogueiraAHombergsmeierEMayMWolfrumJFailure behavior of composite T-joints with novel metallic arrow-pin reinforcementCompos Struct2014110162810.1016/j.compstruct.2013.11.022 – reference: JohnsonGCookWFracture characteristics of three metals subjected to various strains, strain rates, temperatures and pressuresEng Fract Mech1985211314810.1016/0013-7944(85)90052-9 – reference: VarasDLopez-PuenteJZaeraRNumerical analysis of the hydrodynamic ram phenomenon in aircraft fuel tanksAIAA20125071621163010.2514/1.J051613 – reference: Moussa NA, Whale MD, Groszmann DE, Zhang XJ (1997) The potential for fuel tank fire and hydrodynamic ram from uncontained aircraft engine debris. DOT/FAA/AR-96/95, BlazeTech corporation, Cambridge, MA – reference: Lamberson L, Mates S, Eliasson V (2020) Dynamic behavior of materials. Proceedings of the 2020 annual conference on experimental and applied mechanics, vol 1 – reference: Artero-GuerreroJAPernas-SanchezJVarasDLopez-PuenteJNumerical analysis of CFRP fluid-filled tubes subjected to high-velocity impactCompos Struct20139628629710.1016/j.compstruct.2012.09.020 – reference: Gonzalez M, Sparks C, Kubes C, Girard W (2008) Comparison of the tumbling behavior and pressure evolution of several API projectiles in a hydrodynamic ram environment. 49th AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials conference, Schaumburg AIAA 2008-1965:1-15. https://doi.org/10.2514/6.2008-1965 – reference: Flores-JohnsonEShenLNguyenGFinite-element modelling of the impact behaviour of aluminum nacre-like compositeAppl Mech Mater201410.4028/www.scientific.net/AMM.566.457 – reference: Hinrichsen R, Stratton S, Moussa A, Zhang G (2008) Hydrodynamic ram simulator. Joint aircraft survivability program report, JASPO-V-07-06-001, Wright-Patterson, OH – reference: TuckerJNext generation fire modeling, aircraft survivability2017BerlinSpring713 – volume: 110 start-page: 16 year: 2014 ident: 565_CR5 publication-title: Compos Struct doi: 10.1016/j.compstruct.2013.11.022 – ident: 565_CR13 – ident: 565_CR1 doi: 10.2514/6.2008-1965 – volume: 21 start-page: 31 issue: 1 year: 1985 ident: 565_CR8 publication-title: Eng Fract Mech doi: 10.1016/0013-7944(85)90052-9 – year: 2018 ident: 565_CR11 publication-title: Materials doi: 10.3390/ma11060938 – start-page: 7 volume-title: Next generation fire modeling, aircraft survivability year: 2017 ident: 565_CR14 – year: 2014 ident: 565_CR9 publication-title: Appl Mech Mater doi: 10.4028/www.scientific.net/AMM.566.457 – ident: 565_CR2 doi: 10.2514/6.2005-2330 – volume: 50 start-page: 1621 issue: 7 year: 2012 ident: 565_CR6 publication-title: AIAA doi: 10.2514/1.J051613 – ident: 565_CR12 doi: 10.1016/j.procir.2015.04.093 – volume: 96 start-page: 286 year: 2013 ident: 565_CR7 publication-title: Compos Struct doi: 10.1016/j.compstruct.2012.09.020 – ident: 565_CR10 doi: 10.1007/978-3-030-59947-8 – ident: 565_CR4 – ident: 565_CR3 doi: 10.2514/6.2005-7647 |
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| SubjectTerms | Aerospace Technology and Astronautics Engineering Fluid- and Aerodynamics Original Paper 항공우주공학 |
| Title | Ballistic Penetration Test and Simulation of Metallic Aircraft Wing Fuel Tank |
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