In-flight icing on unmanned aerial vehicle and its aerodynamic penalties

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DOIResolve DOI: http://doi.org/10.1051/eucass/2016090173
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TypeArticle
Proceedings titleProgress in Flight Physics. Volume 9
ConferenceProgress in Flight Physics, June 29-July 3, 2015, Krakow, Poland
ISBN978-5-94588-215-7
Pages173188
AbstractA numerical prediction of ice accretion on HQ309, SD7032, and SD7037 airfoils and its aerodynamic penalties is described. Ice accretion prediction on a three-dimensional (3D) swept wing is also presented. In addition to airflow and drop trajectory solvers, NRC's (National Research Council) original, 3D, morphogenetic icing modeling approach has been used. The analysis was performed for a wide range of icing conditions identi¦ed in the FAA (Federal Aviation Administration) Appendix C icing envelope. They cover a range of drop sizes, air temperatures, and liquid water contents. For selected icing conditions, the resulting decrease in lift and increase in drag have been calculated.
Publication date
PublisherThe European Conference for Aero-Space Sciences
LanguageEnglish
AffiliationAerospace; National Research Council Canada
Peer reviewedYes
NPARC number23002255
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Record identifier67897ab8-a48d-4890-9894-f5da44f01211
Record created2017-09-15
Record modified2017-09-15
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