Bell 412 Rotor Flapping Model, Preliminary Convair Aerodynamic Model in Icing Effect, Falcon 20 Wing Contamination, and pEst Program Development (16-month co-op work term)

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TypeTechnical Report
Subjectaerodyamic model; simulation and modeling; rotor flapping model; aerodynamic model in icing effect; wing contamination and parameter estimation
AffiliationNRC Institute for Aerospace Research; National Research Council Canada
Access conditionavailable
Peer reviewedNo
NRC numberFRL-2003-0064
NPARC number8928733
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Record identifier5e6b91d9-08b2-4583-a984-2921ff038587
Record created2009-04-23
Record modified2016-10-03
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