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Flexural Behavior of Aluminum Honeycomb Core Sandwich Structure
This project is concerned with the fabrication and flexural testing of aluminium honey comb sandwich structure which is a special case of composite materials that is fabricated by attaching two thin but stiff skins to a light weight but thick core. The core material is normally low density material...
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Published in: | IOP conference series. Materials Science and Engineering 2017-05, Vol.197 (1), p.12046 |
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description | This project is concerned with the fabrication and flexural testing of aluminium honey comb sandwich structure which is a special case of composite materials that is fabricated by attaching two thin but stiff skins to a light weight but thick core. The core material is normally low density material but its high thickness provide the sandwich composite with high bonding stiffness. Honeycomb core are classified into two types based on the materials and structures. Hexagonal shape has a unique properties i.e has more bonding strength and less formation time based on the cell size and sheet thickness. Sandwich structure exhibit different properties such as high load bearing capacity at low weight and has excellent thermal insulation. By considering the above properties it has tendency to minimize the structural problem. So honey comb sandwich structure is choosed. The core structure has a different applications such as aircraft, ship interiors, construction industries. As there is no proper research on strength characteristics of sandwich structure. So, we use light weight material to desire the strength. There are different parameters involved in this structure i.e cell size, sheet thickness and core height. In this project we considered 3 level of comparison among the 3 different parameters cell size of 4, 6 and 8 mm, sheet thickness of 0.3, 0.5 and 0.7 mm, and core height of 20,25 and 30 mm. In order to reduce the number of experiment we use taguchi design of experiment, and we select the L8 orthogonal array is the best array for this type of situation, which clearly identifies the parameters by independent of material weight to support this we add the minitab software, to identify the main effective plots and regression equation which involves the individual response and corresponding parameters. Aluminium material is used for the fabrication of Honeycomb sandwich structure among the various grades of aluminium we consider the AL6061 which is light weight material and has more strength. By the power press used as forming method we fabricate the honey comb core and stacking the sheets with adhesive as epoxy resin or laser beam welding and sandwich structure will form with two face sheets. Then the specimen is taken to be tested to know the flexural behaviour by the flexural test as 3 point and 4 pont bend test. After testing of two different tests then we get the force vs displacement curve by this we can know the maximum force and by loading configurations |
doi_str_mv | 10.1088/1757-899X/197/1/012046 |
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The core material is normally low density material but its high thickness provide the sandwich composite with high bonding stiffness. Honeycomb core are classified into two types based on the materials and structures. Hexagonal shape has a unique properties i.e has more bonding strength and less formation time based on the cell size and sheet thickness. Sandwich structure exhibit different properties such as high load bearing capacity at low weight and has excellent thermal insulation. By considering the above properties it has tendency to minimize the structural problem. So honey comb sandwich structure is choosed. The core structure has a different applications such as aircraft, ship interiors, construction industries. As there is no proper research on strength characteristics of sandwich structure. So, we use light weight material to desire the strength. There are different parameters involved in this structure i.e cell size, sheet thickness and core height. In this project we considered 3 level of comparison among the 3 different parameters cell size of 4, 6 and 8 mm, sheet thickness of 0.3, 0.5 and 0.7 mm, and core height of 20,25 and 30 mm. In order to reduce the number of experiment we use taguchi design of experiment, and we select the L8 orthogonal array is the best array for this type of situation, which clearly identifies the parameters by independent of material weight to support this we add the minitab software, to identify the main effective plots and regression equation which involves the individual response and corresponding parameters. Aluminium material is used for the fabrication of Honeycomb sandwich structure among the various grades of aluminium we consider the AL6061 which is light weight material and has more strength. By the power press used as forming method we fabricate the honey comb core and stacking the sheets with adhesive as epoxy resin or laser beam welding and sandwich structure will form with two face sheets. Then the specimen is taken to be tested to know the flexural behaviour by the flexural test as 3 point and 4 pont bend test. After testing of two different tests then we get the force vs displacement curve by this we can know the maximum force and by loading configurations and its displacement or deflection then we can calculate flexural stiffness and core shear modulus by the variation of three parameters. Our ultimate aim is to achieve maximum strength by minimum weight.</description><identifier>ISSN: 1757-8981</identifier><identifier>EISSN: 1757-899X</identifier><identifier>DOI: 10.1088/1757-899X/197/1/012046</identifier><language>eng</language><publisher>Bristol: IOP Publishing</publisher><subject>Aluminum ; Bearing capacity ; Bend tests ; Bonding strength ; Composite materials ; Construction industry ; Design of experiments ; Epoxy resins ; Honey ; Honeycomb cores ; Laser beam welding ; Mathematical analysis ; Minimum weight ; Orthogonal arrays ; Parameter identification ; Power presses ; Sandwich structures ; Shear modulus ; Sheets ; Stiffness ; Taguchi methods ; Thermal insulation ; Thickness ; Weight reduction</subject><ispartof>IOP conference series. Materials Science and Engineering, 2017-05, Vol.197 (1), p.12046</ispartof><rights>Published under licence by IOP Publishing Ltd</rights><rights>2017. 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Materials Science and Engineering</title><addtitle>IOP Conf. Ser.: Mater. Sci. Eng</addtitle><description>This project is concerned with the fabrication and flexural testing of aluminium honey comb sandwich structure which is a special case of composite materials that is fabricated by attaching two thin but stiff skins to a light weight but thick core. The core material is normally low density material but its high thickness provide the sandwich composite with high bonding stiffness. Honeycomb core are classified into two types based on the materials and structures. Hexagonal shape has a unique properties i.e has more bonding strength and less formation time based on the cell size and sheet thickness. Sandwich structure exhibit different properties such as high load bearing capacity at low weight and has excellent thermal insulation. By considering the above properties it has tendency to minimize the structural problem. So honey comb sandwich structure is choosed. The core structure has a different applications such as aircraft, ship interiors, construction industries. As there is no proper research on strength characteristics of sandwich structure. So, we use light weight material to desire the strength. There are different parameters involved in this structure i.e cell size, sheet thickness and core height. In this project we considered 3 level of comparison among the 3 different parameters cell size of 4, 6 and 8 mm, sheet thickness of 0.3, 0.5 and 0.7 mm, and core height of 20,25 and 30 mm. In order to reduce the number of experiment we use taguchi design of experiment, and we select the L8 orthogonal array is the best array for this type of situation, which clearly identifies the parameters by independent of material weight to support this we add the minitab software, to identify the main effective plots and regression equation which involves the individual response and corresponding parameters. Aluminium material is used for the fabrication of Honeycomb sandwich structure among the various grades of aluminium we consider the AL6061 which is light weight material and has more strength. By the power press used as forming method we fabricate the honey comb core and stacking the sheets with adhesive as epoxy resin or laser beam welding and sandwich structure will form with two face sheets. Then the specimen is taken to be tested to know the flexural behaviour by the flexural test as 3 point and 4 pont bend test. After testing of two different tests then we get the force vs displacement curve by this we can know the maximum force and by loading configurations and its displacement or deflection then we can calculate flexural stiffness and core shear modulus by the variation of three parameters. Our ultimate aim is to achieve maximum strength by minimum weight.</description><subject>Aluminum</subject><subject>Bearing capacity</subject><subject>Bend tests</subject><subject>Bonding strength</subject><subject>Composite materials</subject><subject>Construction industry</subject><subject>Design of experiments</subject><subject>Epoxy resins</subject><subject>Honey</subject><subject>Honeycomb cores</subject><subject>Laser beam welding</subject><subject>Mathematical analysis</subject><subject>Minimum weight</subject><subject>Orthogonal arrays</subject><subject>Parameter identification</subject><subject>Power presses</subject><subject>Sandwich structures</subject><subject>Shear modulus</subject><subject>Sheets</subject><subject>Stiffness</subject><subject>Taguchi methods</subject><subject>Thermal insulation</subject><subject>Thickness</subject><subject>Weight reduction</subject><issn>1757-8981</issn><issn>1757-899X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2017</creationdate><recordtype>article</recordtype><sourceid>PIMPY</sourceid><recordid>eNqFkE9Lw0AQxRdRsFa_ggS8eInZSTb75yS1tFaoeKiCt2WTbGhKko2brNpvb0KkIgie5sG892b4IXQJ-AYw5wGwmPlciNcABAsgwBBiQo_Q5LA4PmgOp-isbXcYU0YInqDbZak_nVWld6e36r0w1jO5NytdVdSu8lam1vvUVIk3N1Z7G1VnH0W69TaddWnnrD5HJ7kqW33xPafoZbl4nq_89dP9w3y29lOCWecrmvBQRYwRYJBknERYJwJAY8UZH_5ilOksxGnMcxETygVNgQoS9TJPWDRFV2NvY82b020nd8bZuj8pw5iSWBCISO-ioyu1pm2tzmVji0rZvQQsB1hy4CAHJrKHJUGOsPpgOAYL0_w0_xu6_iP0uFn8sskmy6Mv5v53KA</recordid><startdate>20170501</startdate><enddate>20170501</enddate><creator>Matta, Vidyasagar</creator><creator>Suresh Kumar, J</creator><creator>Venkataraviteja, Duddu</creator><creator>Reddy, Guggulla Bharath Kumar</creator><general>IOP Publishing</general><scope>O3W</scope><scope>TSCCA</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>D1I</scope><scope>DWQXO</scope><scope>HCIFZ</scope><scope>KB.</scope><scope>L6V</scope><scope>M7S</scope><scope>PDBOC</scope><scope>PIMPY</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>PTHSS</scope></search><sort><creationdate>20170501</creationdate><title>Flexural Behavior of Aluminum Honeycomb Core Sandwich Structure</title><author>Matta, Vidyasagar ; Suresh Kumar, J ; Venkataraviteja, Duddu ; Reddy, Guggulla Bharath Kumar</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c407t-a6b82a3774171bd8430eb911e0a8788981767ed20c58f9546896c16943468fb73</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2017</creationdate><topic>Aluminum</topic><topic>Bearing capacity</topic><topic>Bend tests</topic><topic>Bonding strength</topic><topic>Composite materials</topic><topic>Construction industry</topic><topic>Design of experiments</topic><topic>Epoxy resins</topic><topic>Honey</topic><topic>Honeycomb cores</topic><topic>Laser beam welding</topic><topic>Mathematical analysis</topic><topic>Minimum weight</topic><topic>Orthogonal arrays</topic><topic>Parameter identification</topic><topic>Power presses</topic><topic>Sandwich structures</topic><topic>Shear modulus</topic><topic>Sheets</topic><topic>Stiffness</topic><topic>Taguchi methods</topic><topic>Thermal insulation</topic><topic>Thickness</topic><topic>Weight reduction</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Matta, Vidyasagar</creatorcontrib><creatorcontrib>Suresh Kumar, J</creatorcontrib><creatorcontrib>Venkataraviteja, Duddu</creatorcontrib><creatorcontrib>Reddy, Guggulla Bharath Kumar</creatorcontrib><collection>Open Access: IOP Publishing Free Content</collection><collection>IOPscience (Open Access)</collection><collection>CrossRef</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central (Alumni)</collection><collection>ProQuest Central</collection><collection>ProQuest Central Essentials</collection><collection>AUTh Library subscriptions: ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Materials Science Collection</collection><collection>ProQuest Central</collection><collection>SciTech Premium Collection</collection><collection>Materials Science Database</collection><collection>ProQuest Engineering Collection</collection><collection>Engineering Database</collection><collection>Materials science collection</collection><collection>Publicly Available Content Database</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><collection>Engineering Collection</collection><jtitle>IOP conference series. Materials Science and Engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Matta, Vidyasagar</au><au>Suresh Kumar, J</au><au>Venkataraviteja, Duddu</au><au>Reddy, Guggulla Bharath Kumar</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Flexural Behavior of Aluminum Honeycomb Core Sandwich Structure</atitle><jtitle>IOP conference series. Materials Science and Engineering</jtitle><addtitle>IOP Conf. Ser.: Mater. Sci. Eng</addtitle><date>2017-05-01</date><risdate>2017</risdate><volume>197</volume><issue>1</issue><spage>12046</spage><pages>12046-</pages><issn>1757-8981</issn><eissn>1757-899X</eissn><abstract>This project is concerned with the fabrication and flexural testing of aluminium honey comb sandwich structure which is a special case of composite materials that is fabricated by attaching two thin but stiff skins to a light weight but thick core. The core material is normally low density material but its high thickness provide the sandwich composite with high bonding stiffness. Honeycomb core are classified into two types based on the materials and structures. Hexagonal shape has a unique properties i.e has more bonding strength and less formation time based on the cell size and sheet thickness. Sandwich structure exhibit different properties such as high load bearing capacity at low weight and has excellent thermal insulation. By considering the above properties it has tendency to minimize the structural problem. So honey comb sandwich structure is choosed. The core structure has a different applications such as aircraft, ship interiors, construction industries. As there is no proper research on strength characteristics of sandwich structure. So, we use light weight material to desire the strength. There are different parameters involved in this structure i.e cell size, sheet thickness and core height. In this project we considered 3 level of comparison among the 3 different parameters cell size of 4, 6 and 8 mm, sheet thickness of 0.3, 0.5 and 0.7 mm, and core height of 20,25 and 30 mm. In order to reduce the number of experiment we use taguchi design of experiment, and we select the L8 orthogonal array is the best array for this type of situation, which clearly identifies the parameters by independent of material weight to support this we add the minitab software, to identify the main effective plots and regression equation which involves the individual response and corresponding parameters. Aluminium material is used for the fabrication of Honeycomb sandwich structure among the various grades of aluminium we consider the AL6061 which is light weight material and has more strength. By the power press used as forming method we fabricate the honey comb core and stacking the sheets with adhesive as epoxy resin or laser beam welding and sandwich structure will form with two face sheets. Then the specimen is taken to be tested to know the flexural behaviour by the flexural test as 3 point and 4 pont bend test. After testing of two different tests then we get the force vs displacement curve by this we can know the maximum force and by loading configurations and its displacement or deflection then we can calculate flexural stiffness and core shear modulus by the variation of three parameters. Our ultimate aim is to achieve maximum strength by minimum weight.</abstract><cop>Bristol</cop><pub>IOP Publishing</pub><doi>10.1088/1757-899X/197/1/012046</doi><tpages>11</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Aluminum Bearing capacity Bend tests Bonding strength Composite materials Construction industry Design of experiments Epoxy resins Honey Honeycomb cores Laser beam welding Mathematical analysis Minimum weight Orthogonal arrays Parameter identification Power presses Sandwich structures Shear modulus Sheets Stiffness Taguchi methods Thermal insulation Thickness Weight reduction |
title | Flexural Behavior of Aluminum Honeycomb Core Sandwich Structure |
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