Wind Tunnel Testing of Unsteady Loads on a Helicopter Fuselage in a Ship Wake

From National Research Council Canada

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Affiliation
  1. National Research Council of Canada. NRC Institute for Aerospace Research
FormatText, Article
Conference23rd Congress of the International Council of the Aeronautical Sciences 9/8/2002 to 9/13/2002, Toronto, Canada
Subjectdynamic interface; ship airwake; helicopter; unsteady loads
Access condition
  • available
  • unclassified
  • unlimited
Peer reviewedYes
NRC numberAL-2002-0053
NPARC number8927303
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Record identifier3a11800e-5232-49c2-ab29-726f3a8fae53
Record created2009-04-23
Record modified2020-04-16
Date modified: