Flight Dynamics Model Development for Turboprop Transport Aircraft Icing Effects Based on Flight Data

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Conference43rd AIAA Aerospace Sciences Meeting and Exhibit, January 10 - 13, 2005
Subjectflight dynamics model; airframe ice accretion effects; natural ice; simulation mathematical model; aircraft performance degradation; stability and control derivative; parameter estimation
PlaceReno, NV USA
AffiliationNRC Institute for Aerospace Research; National Research Council Canada
Access conditionavailable
Peer reviewedNo
NRC numberFRL-2004-0033
NPARC number8926923
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Record identifierecb44e7a-a65b-4b69-988b-ce6fe61bd05a
Record created2009-04-23
Record modified2016-05-09
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