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Prediction of supercooled droplet impingement on helicopter rotor blades

Linkhttp://www.icas.org/icas_archive/ICAS2008/PAPERS/382.PDF
AuthorSearch for: 1; Search for: 1
Affiliation
  1. National Research Council Canada. Aerospace
FormatText, Article
ConferenceICAS 2008 - 26th Congress of International Council of the Aeronautical Sciences, including the 8th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference, September 14-19, 2008, Anchorage, Alaska, United States
Subjecticing; rotorcraft aerodynamics; CFD
Abstract
The 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.
Date published
PublisherInternational Council of the Aeronautical Sciences
In
  • ICAS 2008 CD-ROM Proceedings: 26th Congress of the International Council of the Aeronautical Sciences (ICAS), including the 8th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference, ICAS 2008-2.6.4 (September 2008).
LanguageEnglish
Peer reviewedYes
NPARC number21277286
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Record identifier31cccfdd-5911-4d71-b58d-93d8ba025d2e
Record created2016-02-04
Record modified2026-09-15

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