Prediction of supercooled droplet impingement on helicopter rotor blades

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Proceedings titleICAS 2008 CD-ROM Proceedings
Conference26th Congress of International Council of the Aeronautical Sciences, including the 8th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference, 14-19 September 2008, Anchorage, Alaska, USA
Article numberICAS 2008-2.6.4
Subjecticing; rotorcraft aerodynamics; CFD
AbstractThe objective of this paper is to examine the predictive capability of NRiCe numerical model, applied to ice formation on helicopter rotor blades. The model consists of three components: an airflow solver, a droplet trajectory solver and a morphogenetic ice growth model.
Publication date
AffiliationNational Research Council Canada; Aerospace
Peer reviewedYes
NPARC number21277286
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Record identifier31cccfdd-5911-4d71-b58d-93d8ba025d2e
Record created2016-02-04
Record modified2016-05-09
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