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)

AuthorSearch for: ; Search for:
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
Export citationExport as RIS
Report a correctionReport a correction
Record identifier5e6b91d9-08b2-4583-a984-2921ff038587
Record created2009-04-23
Record modified2016-10-03
Bookmark and share
  • Share this page with Facebook (Opens in a new window)
  • Share this page with Twitter (Opens in a new window)
  • Share this page with Google+ (Opens in a new window)
  • Share this page with Delicious (Opens in a new window)