{"title":"碳纤维复合材料试样设计参数对人工雷击电流耗散和材料热损伤的影响","authors":"Scott L J Millen, Vipin Kumar, A. Murphy","doi":"10.4271/01-16-02-0017","DOIUrl":null,"url":null,"abstract":"Previous artificial lightning strike direct effect research has examined a broad\n range of specimen design parameters. No works have studied how such specimen\n design parameters and electrical boundary conditions impact the dissipation of\n electric current flow through individual plies. This article assesses the\n influence of carbon fiber composite specimen design parameters (design\n parameters = specimen size, shape, and stacking sequence) and electrical\n boundary conditions on the dissipation of current and the spread of damage\n resulting from Joule heating. Thermal-electric finite element (FE) modelling is\n used and laboratory scale (<1 m long) and aircraft scale (>1 m long)\n models are generated in which laminated ply current dissipation is predicted,\n considering a fixed artificial lightning current waveform. The simulation\n results establish a positive correlation between the current exiting the\n specimen from a given ply and the amount of thermal damage in that ply. The\n results also establish that the distance to ground, from the strike location to\n the zero potential boundary conditions (ground), is the controlling factor which\n dictates the electric current dissipation in each ply. Significantly, this\n distance to ground is dependent on each of the specimen shape, dimensions,\n stacking sequence, and location of ground boundary conditions. Therefore, it is\n not possible to decouple current dissipation and damage from specimen design and\n boundary condition setup. However, it is possible to define a specimen size for\n a given specimen shape, stacking sequence, and waveform which limit the\n influence of specimen dimensions on the resulting current distribution and\n damage. For a rectangular specimen design which appears in literature multiple\n times, as 100 × 150 mm and with a stacking sequence of\n [45/0/−45/90]4s, a specimen design of greater than 300 × 200 mm\n is required to limit the influence of specimen dimensions on current\n distribution and damage.","PeriodicalId":44558,"journal":{"name":"SAE International Journal of Aerospace","volume":" ","pages":""},"PeriodicalIF":0.3000,"publicationDate":"2023-04-29","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"The Influence of Carbon Fiber Composite Specimen Design Parameters on\\n Artificial Lightning Strike Current Dissipation and Material Thermal\\n Damage\",\"authors\":\"Scott L J Millen, Vipin Kumar, A. Murphy\",\"doi\":\"10.4271/01-16-02-0017\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Previous artificial lightning strike direct effect research has examined a broad\\n range of specimen design parameters. No works have studied how such specimen\\n design parameters and electrical boundary conditions impact the dissipation of\\n electric current flow through individual plies. This article assesses the\\n influence of carbon fiber composite specimen design parameters (design\\n parameters = specimen size, shape, and stacking sequence) and electrical\\n boundary conditions on the dissipation of current and the spread of damage\\n resulting from Joule heating. Thermal-electric finite element (FE) modelling is\\n used and laboratory scale (<1 m long) and aircraft scale (>1 m long)\\n models are generated in which laminated ply current dissipation is predicted,\\n considering a fixed artificial lightning current waveform. The simulation\\n results establish a positive correlation between the current exiting the\\n specimen from a given ply and the amount of thermal damage in that ply. The\\n results also establish that the distance to ground, from the strike location to\\n the zero potential boundary conditions (ground), is the controlling factor which\\n dictates the electric current dissipation in each ply. Significantly, this\\n distance to ground is dependent on each of the specimen shape, dimensions,\\n stacking sequence, and location of ground boundary conditions. Therefore, it is\\n not possible to decouple current dissipation and damage from specimen design and\\n boundary condition setup. However, it is possible to define a specimen size for\\n a given specimen shape, stacking sequence, and waveform which limit the\\n influence of specimen dimensions on the resulting current distribution and\\n damage. For a rectangular specimen design which appears in literature multiple\\n times, as 100 × 150 mm and with a stacking sequence of\\n [45/0/−45/90]4s, a specimen design of greater than 300 × 200 mm\\n is required to limit the influence of specimen dimensions on current\\n distribution and damage.\",\"PeriodicalId\":44558,\"journal\":{\"name\":\"SAE International Journal of Aerospace\",\"volume\":\" \",\"pages\":\"\"},\"PeriodicalIF\":0.3000,\"publicationDate\":\"2023-04-29\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"SAE International Journal of Aerospace\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.4271/01-16-02-0017\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q4\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"SAE International Journal of Aerospace","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.4271/01-16-02-0017","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q4","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
The Influence of Carbon Fiber Composite Specimen Design Parameters on
Artificial Lightning Strike Current Dissipation and Material Thermal
Damage
Previous artificial lightning strike direct effect research has examined a broad
range of specimen design parameters. No works have studied how such specimen
design parameters and electrical boundary conditions impact the dissipation of
electric current flow through individual plies. This article assesses the
influence of carbon fiber composite specimen design parameters (design
parameters = specimen size, shape, and stacking sequence) and electrical
boundary conditions on the dissipation of current and the spread of damage
resulting from Joule heating. Thermal-electric finite element (FE) modelling is
used and laboratory scale (<1 m long) and aircraft scale (>1 m long)
models are generated in which laminated ply current dissipation is predicted,
considering a fixed artificial lightning current waveform. The simulation
results establish a positive correlation between the current exiting the
specimen from a given ply and the amount of thermal damage in that ply. The
results also establish that the distance to ground, from the strike location to
the zero potential boundary conditions (ground), is the controlling factor which
dictates the electric current dissipation in each ply. Significantly, this
distance to ground is dependent on each of the specimen shape, dimensions,
stacking sequence, and location of ground boundary conditions. Therefore, it is
not possible to decouple current dissipation and damage from specimen design and
boundary condition setup. However, it is possible to define a specimen size for
a given specimen shape, stacking sequence, and waveform which limit the
influence of specimen dimensions on the resulting current distribution and
damage. For a rectangular specimen design which appears in literature multiple
times, as 100 × 150 mm and with a stacking sequence of
[45/0/−45/90]4s, a specimen design of greater than 300 × 200 mm
is required to limit the influence of specimen dimensions on current
distribution and damage.