A Parametric Study of Reversible Jet-Fan Blades Aerodynamic Performance
This paper presents a fully reversible blade parametric design methodology. The blades are for application in jet fans that ventilate and provide emergency smoke control in road tunnels. The blade design variables are tip solidity, twist, and camber distribution. The authors base the design methodol...
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Veröffentlicht in: | Journal of engineering for gas turbines and power 2013-02, Vol.135 (2), p.1-4 |
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description | This paper presents a fully reversible blade parametric design methodology. The blades are for application in jet fans that ventilate and provide emergency smoke control in road tunnels. The blade design variables are tip solidity, twist, and camber distribution. The authors base the design methodology on a sensitivity analysis which they derived from a response surface approximation. They construct the latter using a computational analysis of four experimental cases which they generated using an experimental design approach. The sensitivity analysis calculates a rank and a weight for each design variable that affects the jet-fan performance parameters thrust and efficiency, and thus facilitates insight into each variable's relative importance. Finally, the authors present a redesign of an existing reversible jet-fan blade by following the design guidelines which they obtained from the sensitivity analysis. The authors study the aerodynamic characteristics of the redesigned blade and compare it to that of the baseline design configuration. They then manufacture a redesigned blade prototype. Finally, the authors present thrust and power measurements for both the baseline jet fan, and the baseline jet fan when fitted with a redesigned blade. |
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G</creator><creatorcontrib>Daneshkhah, Kasra ; Sheard, A. G</creatorcontrib><description>This paper presents a fully reversible blade parametric design methodology. The blades are for application in jet fans that ventilate and provide emergency smoke control in road tunnels. The blade design variables are tip solidity, twist, and camber distribution. The authors base the design methodology on a sensitivity analysis which they derived from a response surface approximation. They construct the latter using a computational analysis of four experimental cases which they generated using an experimental design approach. The sensitivity analysis calculates a rank and a weight for each design variable that affects the jet-fan performance parameters thrust and efficiency, and thus facilitates insight into each variable's relative importance. Finally, the authors present a redesign of an existing reversible jet-fan blade by following the design guidelines which they obtained from the sensitivity analysis. The authors study the aerodynamic characteristics of the redesigned blade and compare it to that of the baseline design configuration. They then manufacture a redesigned blade prototype. Finally, the authors present thrust and power measurements for both the baseline jet fan, and the baseline jet fan when fitted with a redesigned blade.</description><identifier>ISSN: 0742-4795</identifier><identifier>EISSN: 1528-8919</identifier><identifier>DOI: 10.1115/1.4007758</identifier><identifier>CODEN: JETPEZ</identifier><language>eng</language><publisher>New York, N: ASME</publisher><subject>Applied sciences ; Blades ; Design engineering ; Emergencies ; Energy ; Energy. 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Finally, the authors present a redesign of an existing reversible jet-fan blade by following the design guidelines which they obtained from the sensitivity analysis. The authors study the aerodynamic characteristics of the redesigned blade and compare it to that of the baseline design configuration. They then manufacture a redesigned blade prototype. Finally, the authors present thrust and power measurements for both the baseline jet fan, and the baseline jet fan when fitted with a redesigned blade.</description><subject>Applied sciences</subject><subject>Blades</subject><subject>Design engineering</subject><subject>Emergencies</subject><subject>Energy</subject><subject>Energy. Thermal use of fuels</subject><subject>Engines and turbines</subject><subject>Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc</subject><subject>Exact sciences and technology</subject><subject>Mathematical analysis</subject><subject>Mathematical models</subject><subject>Methodology</subject><subject>Sensitivity analysis</subject><subject>Thrust</subject><issn>0742-4795</issn><issn>1528-8919</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2013</creationdate><recordtype>article</recordtype><recordid>eNqF0LtPwzAQBnALgUQpDMwsWZBgSPHF8SNjqWgBVaLiMVuOfZFS5QF2gtT_HqNWrEw3fL876T5CLoHOAIDfwSynVEqujsgEeKZSVUBxTCZU5lmay4KfkrMQtpQCY7mckNU82RhvWhx8bZO3YXS7pK-SV_xGH-qyweQZh3RpuuS-MQ5DMkffu11n2sg36Kvet6azeE5OKtMEvDjMKflYPrwvHtP1y-ppMV-nhlE-pJIyYcFxBJ5bqDIsWe4USiEcOloKhWVFLXNl6VSGFqijKheSSZqjLbhiU3Kzv_vp-68Rw6DbOlhsGtNhPwYNQnEFhaDZ_5RntBBRikhv99T6PgSPlf70dWv8TgPVv71q0Ideo70-nDXBmqby8f06_C1kEiTnTEZ3tXcmtKi3_ei7WIyOCYv5D6k-flc</recordid><startdate>20130201</startdate><enddate>20130201</enddate><creator>Daneshkhah, Kasra</creator><creator>Sheard, A. 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Thermal use of fuels</topic><topic>Engines and turbines</topic><topic>Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc</topic><topic>Exact sciences and technology</topic><topic>Mathematical analysis</topic><topic>Mathematical models</topic><topic>Methodology</topic><topic>Sensitivity analysis</topic><topic>Thrust</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Daneshkhah, Kasra</creatorcontrib><creatorcontrib>Sheard, A. 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Gas Turbines Power</stitle><date>2013-02-01</date><risdate>2013</risdate><volume>135</volume><issue>2</issue><spage>1</spage><epage>4</epage><pages>1-4</pages><issn>0742-4795</issn><eissn>1528-8919</eissn><coden>JETPEZ</coden><abstract>This paper presents a fully reversible blade parametric design methodology. The blades are for application in jet fans that ventilate and provide emergency smoke control in road tunnels. The blade design variables are tip solidity, twist, and camber distribution. The authors base the design methodology on a sensitivity analysis which they derived from a response surface approximation. They construct the latter using a computational analysis of four experimental cases which they generated using an experimental design approach. The sensitivity analysis calculates a rank and a weight for each design variable that affects the jet-fan performance parameters thrust and efficiency, and thus facilitates insight into each variable's relative importance. 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subjects | Applied sciences Blades Design engineering Emergencies Energy Energy. Thermal use of fuels Engines and turbines Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc Exact sciences and technology Mathematical analysis Mathematical models Methodology Sensitivity analysis Thrust |
title | A Parametric Study of Reversible Jet-Fan Blades Aerodynamic Performance |
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