Identification of aeroelastic parameters for helicopter tail rotor limit cycle oscillation monitoring

AuthorSearch for: ; Search for: ; Search for:
Proceedings titleInternational Conference on Adaptive Structures and Technologies
ConferenceICAST2014 : 25nd International Conference on Adaptive Structures and Technologies, October 6-8th, 2014, The Hague, The Netherlands
Pages118; # of pages: 18
SubjectAeroelasticity; Aeroservoelasticity; Fighter aircraft; Helicopter rotors; Helicopters; Identification (control systems); Stochastic systems; Vibration analysis; Center frequency; In-situ measurement; Limit Cycle Oscillation
Publication date
AffiliationAerospace; National Research Council Canada
Peer reviewedYes
NPARC number21275938
Export citationExport as RIS
Report a correctionReport a correction
Record identifier9c5804de-d532-4670-8491-4ab06432314a
Record created2015-08-11
Record modified2016-05-09
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)
Date modified: