Validation of a Hot-Air Anti-Icing Simulation Code
This paper presents CHT2D, a 2D hot air anti-icing simulation tool developed by the Advanced Aerodynamics group of Bombardier Aerospace. The tool has been developed from two main modules: the ice prediction code CANICE and the Navier-Stokes solver NSU2D, which is used to solve the hot air internal f...
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| Veröffentlicht in: | SAE transactions 2003-01, Vol.112, p.565-572 |
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| creator | Pueyo, A. Mokhtarian, F. Kafyeke, F. |
| description | This paper presents CHT2D, a 2D hot air anti-icing simulation tool developed by the Advanced Aerodynamics group of Bombardier Aerospace. The tool has been developed from two main modules: the ice prediction code CANICE and the Navier-Stokes solver NSU2D, which is used to solve the hot air internal flow. A "weak" coupling beween the two modules based on function calls and information exchange has been priviledged. Three validation test cases are presented: for dry air conditions. Predictions from CHT2D agree quite well with the experiments. Preliminary results are also presented for a test case in icing conditions for different heat loads from the anti-icing system, to study the effect on the accumulated ice. |
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The tool has been developed from two main modules: the ice prediction code CANICE and the Navier-Stokes solver NSU2D, which is used to solve the hot air internal flow. A "weak" coupling beween the two modules based on function calls and information exchange has been priviledged. Three validation test cases are presented: for dry air conditions. Predictions from CHT2D agree quite well with the experiments. Preliminary results are also presented for a test case in icing conditions for different heat loads from the anti-icing system, to study the effect on the accumulated ice.</description><identifier>ISSN: 0096-736X</identifier><identifier>EISSN: 2577-1531</identifier><language>eng</language><publisher>Society of Automotive Engineers, Inc</publisher><subject>Aircraft wings ; Airfoils ; Bombardiers ; Conductive heat transfer ; Heat ; Ice ; Ice formation ; Internal flow ; Skin temperature ; Temperature distribution</subject><ispartof>SAE transactions, 2003-01, Vol.112, p.565-572</ispartof><rights>Copyright 2004 Society of Automotive Engineers, Inc.</rights><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://www.jstor.org/stable/pdf/44699238$$EPDF$$P50$$Gjstor$$H</linktopdf><linktohtml>$$Uhttps://www.jstor.org/stable/44699238$$EHTML$$P50$$Gjstor$$H</linktohtml><link.rule.ids>314,780,784,803,58017,58250</link.rule.ids></links><search><creatorcontrib>Pueyo, A.</creatorcontrib><creatorcontrib>Mokhtarian, F.</creatorcontrib><creatorcontrib>Kafyeke, F.</creatorcontrib><title>Validation of a Hot-Air Anti-Icing Simulation Code</title><title>SAE transactions</title><description>This paper presents CHT2D, a 2D hot air anti-icing simulation tool developed by the Advanced Aerodynamics group of Bombardier Aerospace. 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Preliminary results are also presented for a test case in icing conditions for different heat loads from the anti-icing system, to study the effect on the accumulated ice.</description><subject>Aircraft wings</subject><subject>Airfoils</subject><subject>Bombardiers</subject><subject>Conductive heat transfer</subject><subject>Heat</subject><subject>Ice</subject><subject>Ice formation</subject><subject>Internal flow</subject><subject>Skin temperature</subject><subject>Temperature distribution</subject><issn>0096-736X</issn><issn>2577-1531</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2003</creationdate><recordtype>article</recordtype><sourceid/><recordid>eNpjYuA0MjU31zU0NTZkYeA0MLA00zU3NovgYOAqLs4yMDA2NDU34mQwCkvMyUxJLMnMz1PIT1NIVPDIL9F1zCxScMwrydT1TM7MS1cIzswtzYEocc5PSeVhYE1LzClO5YXS3Ayybq4hzh66WcUl-UXxBUWZuYlFlfEmJmaWlkbGFsaE5AHbii_v</recordid><startdate>20030101</startdate><enddate>20030101</enddate><creator>Pueyo, A.</creator><creator>Mokhtarian, F.</creator><creator>Kafyeke, F.</creator><general>Society of Automotive Engineers, Inc</general><scope/></search><sort><creationdate>20030101</creationdate><title>Validation of a Hot-Air Anti-Icing Simulation Code</title><author>Pueyo, A. ; Mokhtarian, F. ; Kafyeke, F.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-jstor_primary_446992383</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2003</creationdate><topic>Aircraft wings</topic><topic>Airfoils</topic><topic>Bombardiers</topic><topic>Conductive heat transfer</topic><topic>Heat</topic><topic>Ice</topic><topic>Ice formation</topic><topic>Internal flow</topic><topic>Skin temperature</topic><topic>Temperature distribution</topic><toplevel>online_resources</toplevel><creatorcontrib>Pueyo, A.</creatorcontrib><creatorcontrib>Mokhtarian, F.</creatorcontrib><creatorcontrib>Kafyeke, F.</creatorcontrib><jtitle>SAE transactions</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Pueyo, A.</au><au>Mokhtarian, F.</au><au>Kafyeke, F.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Validation of a Hot-Air Anti-Icing Simulation Code</atitle><jtitle>SAE transactions</jtitle><date>2003-01-01</date><risdate>2003</risdate><volume>112</volume><spage>565</spage><epage>572</epage><pages>565-572</pages><issn>0096-736X</issn><eissn>2577-1531</eissn><abstract>This paper presents CHT2D, a 2D hot air anti-icing simulation tool developed by the Advanced Aerodynamics group of Bombardier Aerospace. 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| fulltext | fulltext |
| identifier | ISSN: 0096-736X |
| ispartof | SAE transactions, 2003-01, Vol.112, p.565-572 |
| issn | 0096-736X 2577-1531 |
| language | eng |
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| source | JSTOR Archive Collection A-Z Listing |
| subjects | Aircraft wings Airfoils Bombardiers Conductive heat transfer Heat Ice Ice formation Internal flow Skin temperature Temperature distribution |
| title | Validation of a Hot-Air Anti-Icing Simulation Code |
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