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Unsteady Flow Simulations past a Bell 412 Helicopter in Hover, Low and High Forward Speeds Using Chimera Grid Technique and Their Comparisons.

From National Research Council Canada

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Affiliation
  1. National Research Council of Canada. NRC Institute for Aerospace Research
FormatText, Abstract
ConferenceThe AHS International 64th Annual Forum & Technology Display from 4/29/2008 to 5/1/2008
SubjectBell 412 Helicopter; Unsteady Flows; CFD; Hover; Forward Flight; Chimera Grid Method
PlaceMontreal, Canada
Access condition
  • available
  • unclassified
  • unlimited
NRC numberAL-2007-0088
NPARC number8931778
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Record identifier46de1f97-3443-483b-beb2-d1c2269377f5
Record created2009-04-23
Record modified2020-03-02
Date modified: