Investigation of Relative Humidity and Induced-Vortex Effects on Aircraft Icing
Two new mechanisms for downstream ice growth (i.e., downstream of the primary ice shape) in aircraft icing scenarios were investigated. The first mechanism is local variation of relative humidity with its potential for water deposition due to supersaturation. The second mechanism is induced-vortex e...
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Veröffentlicht in: | Journal of aircraft 2007-11, Vol.44 (6), p.1805-1814 |
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creator | Ogretim, Egemen O Huebsch, Wade W Narramore, Jim Mullins, Bob |
description | Two new mechanisms for downstream ice growth (i.e., downstream of the primary ice shape) in aircraft icing scenarios were investigated. The first mechanism is local variation of relative humidity with its potential for water deposition due to supersaturation. The second mechanism is induced-vortex effects due to their potential impact on droplet paths. It was shown that for rough surfaces with an extended period of exposure, relative humidity effects can lead to additional growth. The resultant frost is a sandpaperlike roughness that can severely degrade the aerodynamic performance of the wings. It was also shown that the vortices induced by the existing ice-shape features are capable of altering the droplet paths. As a result, impingements occur beyond the limits predicted by the methods in other icing prediction codes. [PUBLICATION ABSTRACT] |
doi_str_mv | 10.2514/1.28794 |
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The first mechanism is local variation of relative humidity with its potential for water deposition due to supersaturation. The second mechanism is induced-vortex effects due to their potential impact on droplet paths. It was shown that for rough surfaces with an extended period of exposure, relative humidity effects can lead to additional growth. The resultant frost is a sandpaperlike roughness that can severely degrade the aerodynamic performance of the wings. It was also shown that the vortices induced by the existing ice-shape features are capable of altering the droplet paths. As a result, impingements occur beyond the limits predicted by the methods in other icing prediction codes. 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[PUBLICATION ABSTRACT]</description><subject>Aerodynamics</subject><subject>Air transportation and traffic</subject><subject>Aircraft</subject><subject>Applied sciences</subject><subject>Design engineering</subject><subject>Exact sciences and technology</subject><subject>Ground, air and sea transportation, marine construction</subject><subject>Humidity</subject><issn>0021-8669</issn><issn>1533-3868</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2007</creationdate><recordtype>article</recordtype><recordid>eNpt0MtKAzEUBuAgCtYqvsIgXnAxmusksyzipSAIom7DaS4lZTpTkxnRtzfaglBcJYsv_8n5ETom-IoKwq_JFVWy5jtoRARjJVOV2kUjjCkpVVXV--ggpQXGWGEpR-hp2n641Ic59KFri84Xz67J9w9XPAzLYEP_VUBri2lrB-Ns-dbF3n0Wt94706ciP5mEaCL4vpia0M4P0Z6HJrmjzTlGr3e3LzcP5ePT_fRm8lgCk1VfOmVrwTlVM-kJYRI4dUYKQWaKYsP4jALMai6qykigtfAWKxDGGSIE89ayMTpf565i9z7kDfQyJOOaBlrXDUkzwgmnnGZ4sgUX3RDb_DdNsawwr5jK6GKNTOxSis7rVQxLiF-aYP3Tqib6t9UszzZxkAw0PkJrQvrjdc2pUHV2l2sHAeBv5CZGr6zXfmia3GWf7em_dmv0N_8Jjvc</recordid><startdate>20071101</startdate><enddate>20071101</enddate><creator>Ogretim, Egemen O</creator><creator>Huebsch, Wade W</creator><creator>Narramore, Jim</creator><creator>Mullins, Bob</creator><general>American Institute of Aeronautics and Astronautics</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope><scope>U9A</scope></search><sort><creationdate>20071101</creationdate><title>Investigation of Relative Humidity and Induced-Vortex Effects on Aircraft Icing</title><author>Ogretim, Egemen O ; Huebsch, Wade W ; Narramore, Jim ; Mullins, Bob</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a376t-e8d954428b7f1137a42ec7551b820c34b2aab94566c7a295fd08a5cec1553fdd3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2007</creationdate><topic>Aerodynamics</topic><topic>Air transportation and traffic</topic><topic>Aircraft</topic><topic>Applied sciences</topic><topic>Design engineering</topic><topic>Exact sciences and technology</topic><topic>Ground, air and sea transportation, marine construction</topic><topic>Humidity</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Ogretim, Egemen O</creatorcontrib><creatorcontrib>Huebsch, Wade W</creatorcontrib><creatorcontrib>Narramore, Jim</creatorcontrib><creatorcontrib>Mullins, Bob</creatorcontrib><collection>Pascal-Francis</collection><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><jtitle>Journal of aircraft</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Ogretim, Egemen O</au><au>Huebsch, Wade W</au><au>Narramore, Jim</au><au>Mullins, Bob</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Investigation of Relative Humidity and Induced-Vortex Effects on Aircraft Icing</atitle><jtitle>Journal of aircraft</jtitle><date>2007-11-01</date><risdate>2007</risdate><volume>44</volume><issue>6</issue><spage>1805</spage><epage>1814</epage><pages>1805-1814</pages><issn>0021-8669</issn><eissn>1533-3868</eissn><coden>JAIRAM</coden><abstract>Two new mechanisms for downstream ice growth (i.e., downstream of the primary ice shape) in aircraft icing scenarios were investigated. 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subjects | Aerodynamics Air transportation and traffic Aircraft Applied sciences Design engineering Exact sciences and technology Ground, air and sea transportation, marine construction Humidity |
title | Investigation of Relative Humidity and Induced-Vortex Effects on Aircraft Icing |
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