Technique for Evaluating the Strength of Composite Blades
The paper presents a technique for designing and investigating the strength of a composite blade on an example of a mine ore ventilation fan, considering aerodynamic loads acting on a blade airfoil surface. The technique is based on the use of the finite element method in a combination with the theo...
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Veröffentlicht in: | Journal of the Institution of Engineers (India) Series C 2020-06, Vol.101 (3), p.451-461 |
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creator | Martynenko, Volodymyr Hrytsenko, Mykyta Martynenko, Gennadii |
description | The paper presents a technique for designing and investigating the strength of a composite blade on an example of a mine ore ventilation fan, considering aerodynamic loads acting on a blade airfoil surface. The technique is based on the use of the finite element method in a combination with the theory of multilayer shells to determine the dynamics and strength of the composite airfoil, as well as the methods of the computational fluid dynamics, namely the Reynolds equations, for modeling an air movement in a fan passage to determine aerodynamic loads. A static strength estimation is based on an application of the Hashin strength criterion. An analysis of the results of strength calculations considering aerodynamic forces indicates a necessity of accounting them for thin-walled composite elements. A possibility of varying a thickness of the shell and taking it into account using the presented method allows to achieve an optimal ratio of strength and weight indices. A buckling analysis of the composite shell under an action of complex loading, based on methods of the linear stability theory, as well as calculations of natural frequencies and natural frequencies with regard to a prestressed state from an action of static loads, completes the technique. The results of the research allow to conclude on an applicability of the presented methodology for analyzing the strength of composite blades and an efficiency of the proposed design of the airfoil, as well as a possibility of its use to create real rotary machines. |
doi_str_mv | 10.1007/s40032-020-00572-9 |
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The technique is based on the use of the finite element method in a combination with the theory of multilayer shells to determine the dynamics and strength of the composite airfoil, as well as the methods of the computational fluid dynamics, namely the Reynolds equations, for modeling an air movement in a fan passage to determine aerodynamic loads. A static strength estimation is based on an application of the Hashin strength criterion. An analysis of the results of strength calculations considering aerodynamic forces indicates a necessity of accounting them for thin-walled composite elements. A possibility of varying a thickness of the shell and taking it into account using the presented method allows to achieve an optimal ratio of strength and weight indices. A buckling analysis of the composite shell under an action of complex loading, based on methods of the linear stability theory, as well as calculations of natural frequencies and natural frequencies with regard to a prestressed state from an action of static loads, completes the technique. The results of the research allow to conclude on an applicability of the presented methodology for analyzing the strength of composite blades and an efficiency of the proposed design of the airfoil, as well as a possibility of its use to create real rotary machines.</description><identifier>ISSN: 2250-0545</identifier><identifier>EISSN: 2250-0553</identifier><identifier>DOI: 10.1007/s40032-020-00572-9</identifier><language>eng</language><publisher>New Delhi: Springer India</publisher><subject>Aerodynamic forces ; Aerodynamic loads ; Aerodynamics ; Aerospace Technology and Astronautics ; Blades ; Composite structures ; Computational fluid dynamics ; Engineering ; Finite element method ; Industrial and Production Engineering ; Mechanical Engineering ; Mine ventilation ; Multilayers ; Original Contribution ; Resonant frequencies ; Rotary machines ; Shells (structural forms) ; Static loads ; Strength</subject><ispartof>Journal of the Institution of Engineers (India) Series C, 2020-06, Vol.101 (3), p.451-461</ispartof><rights>The Institution of Engineers (India) 2020</rights><rights>The Institution of Engineers (India) 2020.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c2349-830e2aba9695a4da33714dd3ffc055828594236d4a47d301ab24bc6587d5a8a93</citedby><cites>FETCH-LOGICAL-c2349-830e2aba9695a4da33714dd3ffc055828594236d4a47d301ab24bc6587d5a8a93</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.1007/s40032-020-00572-9$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.1007/s40032-020-00572-9$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>314,778,782,27907,27908,41471,42540,51302</link.rule.ids></links><search><creatorcontrib>Martynenko, Volodymyr</creatorcontrib><creatorcontrib>Hrytsenko, Mykyta</creatorcontrib><creatorcontrib>Martynenko, Gennadii</creatorcontrib><title>Technique for Evaluating the Strength of Composite Blades</title><title>Journal of the Institution of Engineers (India) Series C</title><addtitle>J. Inst. Eng. India Ser. C</addtitle><description>The paper presents a technique for designing and investigating the strength of a composite blade on an example of a mine ore ventilation fan, considering aerodynamic loads acting on a blade airfoil surface. The technique is based on the use of the finite element method in a combination with the theory of multilayer shells to determine the dynamics and strength of the composite airfoil, as well as the methods of the computational fluid dynamics, namely the Reynolds equations, for modeling an air movement in a fan passage to determine aerodynamic loads. A static strength estimation is based on an application of the Hashin strength criterion. An analysis of the results of strength calculations considering aerodynamic forces indicates a necessity of accounting them for thin-walled composite elements. A possibility of varying a thickness of the shell and taking it into account using the presented method allows to achieve an optimal ratio of strength and weight indices. A buckling analysis of the composite shell under an action of complex loading, based on methods of the linear stability theory, as well as calculations of natural frequencies and natural frequencies with regard to a prestressed state from an action of static loads, completes the technique. The results of the research allow to conclude on an applicability of the presented methodology for analyzing the strength of composite blades and an efficiency of the proposed design of the airfoil, as well as a possibility of its use to create real rotary machines.</description><subject>Aerodynamic forces</subject><subject>Aerodynamic loads</subject><subject>Aerodynamics</subject><subject>Aerospace Technology and Astronautics</subject><subject>Blades</subject><subject>Composite structures</subject><subject>Computational fluid dynamics</subject><subject>Engineering</subject><subject>Finite element method</subject><subject>Industrial and Production Engineering</subject><subject>Mechanical Engineering</subject><subject>Mine ventilation</subject><subject>Multilayers</subject><subject>Original Contribution</subject><subject>Resonant frequencies</subject><subject>Rotary machines</subject><subject>Shells (structural forms)</subject><subject>Static loads</subject><subject>Strength</subject><issn>2250-0545</issn><issn>2250-0553</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2020</creationdate><recordtype>article</recordtype><recordid>eNp9kM1LAzEQxYMoWGr_AU8Bz6uTr93NUUu1QsGD9Rymm-xHaTc12Qr-96au6M3TzMB7bx4_Qq4Z3DKA4i5KAMEz4JABqIJn-oxMOFfpVEqc_-5SXZJZjFsAYEUuudYToteuavvu_eho7QNdfODuiEPXN3RoHX0dguuboaW-pnO_P_jYDY4-7NC6eEUuatxFN_uZU_L2uFjPl9nq5el5fr_KKi6kzkoBjuMGda4VSotCFExaK-q6Su1KXiotucitRFlYAQw3XG6qXJWFVViiFlNyM-Yegk8142C2_hj69NJwySQwrVWeVHxUVcHHGFxtDqHbY_g0DMyJkhkpmUTJfFMyp2gxmmIS940Lf9H_uL4AUitn6A</recordid><startdate>20200601</startdate><enddate>20200601</enddate><creator>Martynenko, Volodymyr</creator><creator>Hrytsenko, Mykyta</creator><creator>Martynenko, Gennadii</creator><general>Springer India</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope></search><sort><creationdate>20200601</creationdate><title>Technique for Evaluating the Strength of Composite Blades</title><author>Martynenko, Volodymyr ; Hrytsenko, Mykyta ; Martynenko, Gennadii</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c2349-830e2aba9695a4da33714dd3ffc055828594236d4a47d301ab24bc6587d5a8a93</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2020</creationdate><topic>Aerodynamic forces</topic><topic>Aerodynamic loads</topic><topic>Aerodynamics</topic><topic>Aerospace Technology and Astronautics</topic><topic>Blades</topic><topic>Composite structures</topic><topic>Computational fluid dynamics</topic><topic>Engineering</topic><topic>Finite element method</topic><topic>Industrial and Production Engineering</topic><topic>Mechanical Engineering</topic><topic>Mine ventilation</topic><topic>Multilayers</topic><topic>Original Contribution</topic><topic>Resonant frequencies</topic><topic>Rotary machines</topic><topic>Shells (structural forms)</topic><topic>Static loads</topic><topic>Strength</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Martynenko, Volodymyr</creatorcontrib><creatorcontrib>Hrytsenko, Mykyta</creatorcontrib><creatorcontrib>Martynenko, Gennadii</creatorcontrib><collection>CrossRef</collection><jtitle>Journal of the Institution of Engineers (India) Series C</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Martynenko, Volodymyr</au><au>Hrytsenko, Mykyta</au><au>Martynenko, Gennadii</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Technique for Evaluating the Strength of Composite Blades</atitle><jtitle>Journal of the Institution of Engineers (India) Series C</jtitle><stitle>J. Inst. Eng. India Ser. C</stitle><date>2020-06-01</date><risdate>2020</risdate><volume>101</volume><issue>3</issue><spage>451</spage><epage>461</epage><pages>451-461</pages><issn>2250-0545</issn><eissn>2250-0553</eissn><abstract>The paper presents a technique for designing and investigating the strength of a composite blade on an example of a mine ore ventilation fan, considering aerodynamic loads acting on a blade airfoil surface. The technique is based on the use of the finite element method in a combination with the theory of multilayer shells to determine the dynamics and strength of the composite airfoil, as well as the methods of the computational fluid dynamics, namely the Reynolds equations, for modeling an air movement in a fan passage to determine aerodynamic loads. A static strength estimation is based on an application of the Hashin strength criterion. An analysis of the results of strength calculations considering aerodynamic forces indicates a necessity of accounting them for thin-walled composite elements. A possibility of varying a thickness of the shell and taking it into account using the presented method allows to achieve an optimal ratio of strength and weight indices. A buckling analysis of the composite shell under an action of complex loading, based on methods of the linear stability theory, as well as calculations of natural frequencies and natural frequencies with regard to a prestressed state from an action of static loads, completes the technique. The results of the research allow to conclude on an applicability of the presented methodology for analyzing the strength of composite blades and an efficiency of the proposed design of the airfoil, as well as a possibility of its use to create real rotary machines.</abstract><cop>New Delhi</cop><pub>Springer India</pub><doi>10.1007/s40032-020-00572-9</doi><tpages>11</tpages></addata></record> |
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subjects | Aerodynamic forces Aerodynamic loads Aerodynamics Aerospace Technology and Astronautics Blades Composite structures Computational fluid dynamics Engineering Finite element method Industrial and Production Engineering Mechanical Engineering Mine ventilation Multilayers Original Contribution Resonant frequencies Rotary machines Shells (structural forms) Static loads Strength |
title | Technique for Evaluating the Strength of Composite Blades |
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