Flight Dynamics Model of Turboprop Transportation Aircraft Icing Effects Based on Preliminary Flight Data

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TypeArticle
Conference43rd AIAA Aerospace Sciences Meeting and Exhibit, January 10-13, 2005, Reno, NV (USA)
Subjectaircraft simulation and model in natural icing effects; stability and control derivatives; aircraft degradation due to ice accretion; liquid water content; meridian volumetric diameter; aircraft icing model
AffiliationNRC Institute for Aerospace Research; National Research Council Canada
Access conditionavailable
unclassified
unlimited
Peer reviewedYes
NRC numberFRL-2004-0069
NPARC number8931267
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Record identifier82148c32-a6c8-41c8-9f08-d554dff2ba48
Record created2009-04-23
Record modified2016-05-09
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