Recent developments in scaling methods for icing wind tunnel testing at reduced scale

AuthorSearch for: ; Search for:
Proceedings title23rd International Congress of Aeronautical Sciences (ICAS 2002)
Conference23rd International Congress of Aeronautical Sciences (ICAS 2002), Sept. 8-13, 2002, Toronto, Ontario, Canada
Subjecticing testing; reduced scale; scaling methods
AbstractThis paper is concerned with reduced scale testing of in-flight ice accretion on aircraft surfaces. A basic description of the icing process is presented and the reason for occurrence of two types of icing, rime and glaze, is explained. Important physical phenomena are highlighted, including phenomena whose importance is not widely recognized. The implied modelling requirements are outlined and discussed. It is shown that the requirements can be readily satisfied for rime icing conditions and that good reduced scale test results can be obtained. For glaze icing on the other hand, not all of the scaling requirements are known. Recent developments in this area are outlined and discussed in the light of experimental results obtained by the authors and others.
Publication date
PublisherInternational Council of the Aeronautical Sciences
AffiliationNational Research Council Canada; NRC Institute for Aerospace Research
Access conditionavailable
Peer reviewedYes
NRC numberAL-2002-0047
NPARC number8929822
Export citationExport as RIS
Report a correctionReport a correction
Record identifier08d3000c-d739-4879-a268-e057e00ed0c8
Record created2009-04-23
Record modified2016-05-09
Bookmark and share
  • Share this page with Facebook (Opens in a new window)
  • Share this page with Twitter (Opens in a new window)
  • Share this page with Google+ (Opens in a new window)
  • Share this page with Delicious (Opens in a new window)