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

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  1. National Research Council of Canada. Aerospace
FormatText, Article
ConferenceICAST2014: 25nd International Conference on Adaptive Structures and Technologies, October 6-8th, 2014, The Hague, The Netherlands
SubjectAeroelasticity; Aeroservoelasticity; Aeroservoelasticity; Fighter aircraft; Helicopter rotors; Helicopters; Identification (control systems); Stochastic systems; Vibration analysis; Center frequency; In-situ measurement; Limit Cycle Oscillation
Publication date
PublisherETH Zurich / Curran Associates
Peer reviewedYes
NPARC number21275938
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Record identifier9c5804de-d532-4670-8491-4ab06432314a
Record created2015-08-11
Record modified2020-04-22
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