Revisiting Froude’s Theory for Hovering Shrouded Rotor
This paper extends Froude’s momentum theory for free propellers to the analysis of shrouded rotors. A one-dimensional analytical approach is provided, and a homokinetic normal inlet surface model is proposed. Formulations of thrusts and power for each system component are derived, leading to the def...
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Veröffentlicht in: | AIAA journal 2015-07, Vol.53 (7), p.1836-1844 |
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description | This paper extends Froude’s momentum theory for free propellers to the analysis of shrouded rotors. A one-dimensional analytical approach is provided, and a homokinetic normal inlet surface model is proposed. Formulations of thrusts and power for each system component are derived, leading to the definition of optimum design criteria and providing insight into the global aerodynamics of shrouded rotors. In the context of micro-air vehicles applications, assessment of the model is conducted with respect to numerical data. Overall, comparison between numerical and analytical results shows good agreement and highlights the sensitivity of the model to viscous effects. |
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A one-dimensional analytical approach is provided, and a homokinetic normal inlet surface model is proposed. Formulations of thrusts and power for each system component are derived, leading to the definition of optimum design criteria and providing insight into the global aerodynamics of shrouded rotors. In the context of micro-air vehicles applications, assessment of the model is conducted with respect to numerical data. Overall, comparison between numerical and analytical results shows good agreement and highlights the sensitivity of the model to viscous effects.</description><identifier>ISSN: 0001-1452</identifier><identifier>EISSN: 1533-385X</identifier><identifier>DOI: 10.2514/1.J053507</identifier><language>eng</language><publisher>Virginia: American Institute of Aeronautics and Astronautics</publisher><subject>Aerodynamics ; Aerospace engineering ; Assessments ; Automatic ; Design engineering ; Dimensional analysis ; Engineering Sciences ; Hovering ; Inlets ; Mathematical analysis ; Mathematical models ; Micro air vehicles (MAV) ; Momentum theory ; Optimization ; Propellers ; Rotors ; Thrust ; Viscosity</subject><ispartof>AIAA journal, 2015-07, Vol.53 (7), p.1836-1844</ispartof><rights>Copyright © 2014 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. 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Copies of this paper may be made for personal or internal use, on condition that the copier pay the $10.00 per-copy fee to the Copyright Clearance Center, Inc., 222 Rosewood Drive, Danvers, MA 01923; include the code 1533-385X/15 and $10.00 in correspondence with the CCC.</rights><rights>Distributed under a Creative Commons Attribution 4.0 International License</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a418t-baa3aa80a49dea9ea6d09272c3cb6b89b1bb800bea28782e388d8bf37c84a9a43</citedby><cites>FETCH-LOGICAL-a418t-baa3aa80a49dea9ea6d09272c3cb6b89b1bb800bea28782e388d8bf37c84a9a43</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,314,780,784,885,27924,27925</link.rule.ids><backlink>$$Uhttps://hal.science/hal-01131305$$DView record in HAL$$Hfree_for_read</backlink></links><search><creatorcontrib>Jardin, T</creatorcontrib><creatorcontrib>Grondin, G</creatorcontrib><creatorcontrib>Gressier, J</creatorcontrib><creatorcontrib>Huo, C</creatorcontrib><creatorcontrib>Doué, N</creatorcontrib><creatorcontrib>Barènes, R</creatorcontrib><title>Revisiting Froude’s Theory for Hovering Shrouded Rotor</title><title>AIAA journal</title><description>This paper extends Froude’s momentum theory for free propellers to the analysis of shrouded rotors. A one-dimensional analytical approach is provided, and a homokinetic normal inlet surface model is proposed. Formulations of thrusts and power for each system component are derived, leading to the definition of optimum design criteria and providing insight into the global aerodynamics of shrouded rotors. In the context of micro-air vehicles applications, assessment of the model is conducted with respect to numerical data. Overall, comparison between numerical and analytical results shows good agreement and highlights the sensitivity of the model to viscous effects.</description><subject>Aerodynamics</subject><subject>Aerospace engineering</subject><subject>Assessments</subject><subject>Automatic</subject><subject>Design engineering</subject><subject>Dimensional analysis</subject><subject>Engineering Sciences</subject><subject>Hovering</subject><subject>Inlets</subject><subject>Mathematical analysis</subject><subject>Mathematical models</subject><subject>Micro air vehicles (MAV)</subject><subject>Momentum theory</subject><subject>Optimization</subject><subject>Propellers</subject><subject>Rotors</subject><subject>Thrust</subject><subject>Viscosity</subject><issn>0001-1452</issn><issn>1533-385X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2015</creationdate><recordtype>article</recordtype><recordid>eNp9kcFKw0AQhhdRsFYPvkFAED2k7uwmzeyxFGuVglAreFsmycamtN262xR68zV8PZ_E1BYpCp6Gmf_j5x9-xs6Bt0QM0Q20HngsY54csAbEUoYS45dD1uCcQwhRLI7ZifeTehMJQoPh0KxKXy7L-WvQc7bKzef7hw9GY2PdOiisC_p2ZdxGfhp_63kwtEvrTtlRQVNvznazyZ57t6NuPxw83t13O4OQIsBlmBJJIuQUqdyQMtTOuRKJyGSWtlNUKaQpcp4aEpigMBIxx7SQSYYRKYpkk11vfcc01QtXzsittaVS9zsDvblxAAmSxyuo2astu3D2rTJ-qWelz8x0SnNjK68h4SqRqDjW6MUvdGIrN68_0SJStSNGIv6Pgja2gStM9iJmznrvTPGTE7jetKJB71qp2cstSyXRntsf8AtAbYhu</recordid><startdate>20150701</startdate><enddate>20150701</enddate><creator>Jardin, T</creator><creator>Grondin, G</creator><creator>Gressier, J</creator><creator>Huo, C</creator><creator>Doué, N</creator><creator>Barènes, R</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope><scope>1XC</scope><scope>VOOES</scope></search><sort><creationdate>20150701</creationdate><title>Revisiting Froude’s Theory for Hovering Shrouded Rotor</title><author>Jardin, T ; Grondin, G ; Gressier, J ; Huo, C ; Doué, N ; Barènes, R</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a418t-baa3aa80a49dea9ea6d09272c3cb6b89b1bb800bea28782e388d8bf37c84a9a43</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2015</creationdate><topic>Aerodynamics</topic><topic>Aerospace engineering</topic><topic>Assessments</topic><topic>Automatic</topic><topic>Design engineering</topic><topic>Dimensional analysis</topic><topic>Engineering Sciences</topic><topic>Hovering</topic><topic>Inlets</topic><topic>Mathematical analysis</topic><topic>Mathematical models</topic><topic>Micro air vehicles (MAV)</topic><topic>Momentum theory</topic><topic>Optimization</topic><topic>Propellers</topic><topic>Rotors</topic><topic>Thrust</topic><topic>Viscosity</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Jardin, T</creatorcontrib><creatorcontrib>Grondin, G</creatorcontrib><creatorcontrib>Gressier, J</creatorcontrib><creatorcontrib>Huo, C</creatorcontrib><creatorcontrib>Doué, N</creatorcontrib><creatorcontrib>Barènes, R</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Hyper Article en Ligne (HAL)</collection><collection>Hyper Article en Ligne (HAL) (Open Access)</collection><jtitle>AIAA journal</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Jardin, T</au><au>Grondin, G</au><au>Gressier, J</au><au>Huo, C</au><au>Doué, N</au><au>Barènes, R</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Revisiting Froude’s Theory for Hovering Shrouded Rotor</atitle><jtitle>AIAA journal</jtitle><date>2015-07-01</date><risdate>2015</risdate><volume>53</volume><issue>7</issue><spage>1836</spage><epage>1844</epage><pages>1836-1844</pages><issn>0001-1452</issn><eissn>1533-385X</eissn><abstract>This paper extends Froude’s momentum theory for free propellers to the analysis of shrouded rotors. A one-dimensional analytical approach is provided, and a homokinetic normal inlet surface model is proposed. Formulations of thrusts and power for each system component are derived, leading to the definition of optimum design criteria and providing insight into the global aerodynamics of shrouded rotors. In the context of micro-air vehicles applications, assessment of the model is conducted with respect to numerical data. Overall, comparison between numerical and analytical results shows good agreement and highlights the sensitivity of the model to viscous effects.</abstract><cop>Virginia</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.J053507</doi><tpages>9</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Aerodynamics Aerospace engineering Assessments Automatic Design engineering Dimensional analysis Engineering Sciences Hovering Inlets Mathematical analysis Mathematical models Micro air vehicles (MAV) Momentum theory Optimization Propellers Rotors Thrust Viscosity |
title | Revisiting Froude’s Theory for Hovering Shrouded Rotor |
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