AW169 loss of tail rotor effectiveness simulation

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dc.contributor.author Ragazzi, A.
dc.contributor.author Bianco Mengotti, R.
dc.contributor.author Sabato, P.
dc.contributor.author Afruni, G.
dc.contributor.author Hyder, C.
dc.date.accessioned 2020-11-19T15:40:55Z
dc.date.available 2020-11-19T15:40:55Z
dc.date.issued 2017
dc.description.abstract This paper presents the simulation work done to define the rotorcraft flight manual emergency procedure for a loss of tail rotor effectiveness for the AW169 helicopter. The work makes extensive use of both off-line and pilot-in-the-loop simulations.
dc.identifier.other 688_ERF2017
dc.identifier.uri http://hdl.handle.net/20.500.11881/3888
dc.language.iso en
dc.title AW169 loss of tail rotor effectiveness simulation
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