Investigation on the dynamic properties of propeller structure with different number of blades
A propeller is mainly used for propelling the movement for an aircraft or ship. As it gives major contribution towards the performance of an aircraft or ship, study on propeller structure has become popular. In this study, the dynamic or modal characteristics of propeller structure with different nu...
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| Veröffentlicht in: | IOP conference series. Materials Science and Engineering 2020-03, Vol.807 (1), p.12035 |
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| container_title | IOP conference series. Materials Science and Engineering |
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| creator | Abdullah, N.A.Z. Brapakaran, P. Sani, M.S.M. Marcel, M.W. Agung, E.H. |
| description | A propeller is mainly used for propelling the movement for an aircraft or ship. As it gives major contribution towards the performance of an aircraft or ship, study on propeller structure has become popular. In this study, the dynamic or modal characteristics of propeller structure with different number of blade of the same design are investigated. Modal properties of two blades, three blades and four blades propeller that are obtained through computational analysis are compared after validation of three blades propeller is conducted. It has been observed that the four blades propeller has the lowest nominal value of natural frequencies and shows most mode shapes deflection. The results confirm that as the propeller has more number of blades, it will produce more energy and hence has lower natural frequency. |
| doi_str_mv | 10.1088/1757-899X/807/1/012035 |
| format | Article |
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As it gives major contribution towards the performance of an aircraft or ship, study on propeller structure has become popular. In this study, the dynamic or modal characteristics of propeller structure with different number of blade of the same design are investigated. Modal properties of two blades, three blades and four blades propeller that are obtained through computational analysis are compared after validation of three blades propeller is conducted. It has been observed that the four blades propeller has the lowest nominal value of natural frequencies and shows most mode shapes deflection. 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The results confirm that as the propeller has more number of blades, it will produce more energy and hence has lower natural frequency.</description><subject>Aircraft</subject><subject>Aircraft performance</subject><subject>Blades</subject><subject>Resonant frequencies</subject><issn>1757-8981</issn><issn>1757-899X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2020</creationdate><recordtype>article</recordtype><sourceid>O3W</sourceid><sourceid>BENPR</sourceid><recordid>eNqFkF1LwzAUhosoOKd_QQLeeFObzza9lDF1MPFCBa8MbT5cRtfWJFX2782oTARBCCThvM85yZMk5wheIch5hgpWpLwsXzIOiwxlEGFI2EEy2RcO92eOjpMT79cQ5gWlcJK8LtoP7YN9q4LtWhBXWGmgtm21sRL0ruu1C1Z70Jnx1jTaAR_cIMPgNPi0YQWUNUY73QbQDps61mO4biql_WlyZKrG67PvfZo838yfZnfp8uF2MbteppJgzFJSUVpjpZRmtGZGEsKpyo00sFAVxCyHslSEoTJnUNY4Z5QxjjjXdVFEBRWZJhdj3_jG9yF-SKy7wbVxpIg0xiVCtIypfExJ13nvtBG9s5vKbQWCYudS7DSJnTIRXQokRpcRxCNou_6n87_Q5R_Q_eP8V0z0ypAvcHiEWQ</recordid><startdate>20200301</startdate><enddate>20200301</enddate><creator>Abdullah, N.A.Z.</creator><creator>Brapakaran, P.</creator><creator>Sani, M.S.M.</creator><creator>Marcel, M.W.</creator><creator>Agung, E.H.</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>20200301</creationdate><title>Investigation on the dynamic properties of propeller structure with different number of blades</title><author>Abdullah, N.A.Z. ; Brapakaran, P. ; Sani, M.S.M. ; Marcel, M.W. ; Agung, E.H.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c3225-3a44b2ddde54b5fc3384d6fcf07da02560c9d3519650cb2654558188eb77088a3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2020</creationdate><topic>Aircraft</topic><topic>Aircraft performance</topic><topic>Blades</topic><topic>Resonant frequencies</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Abdullah, N.A.Z.</creatorcontrib><creatorcontrib>Brapakaran, P.</creatorcontrib><creatorcontrib>Sani, M.S.M.</creatorcontrib><creatorcontrib>Marcel, M.W.</creatorcontrib><creatorcontrib>Agung, E.H.</creatorcontrib><collection>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 Edition)</collection><collection>ProQuest Central UK/Ireland</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Materials Science Collection</collection><collection>ProQuest Central Korea</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. 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| subjects | Aircraft Aircraft performance Blades Resonant frequencies |
| title | Investigation on the dynamic properties of propeller structure with different number of blades |
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