AW169 loss of tail rotor effectiveness simulation

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dc.contributor.authorRagazzi, A.
dc.contributor.authorBianco Mengotti, R.
dc.contributor.authorSabato, P.
dc.contributor.authorAfruni, G.
dc.contributor.authorHyder, C.
dc.date.accessioned2020-11-19T15:40:55Z
dc.date.available2020-11-19T15:40:55Z
dc.date.issued2017
dc.description.abstractThis 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.other688_ERF2017
dc.identifier.urihttp://hdl.handle.net/20.500.11881/3888
dc.language.isoen
dc.titleAW169 loss of tail rotor effectiveness simulation

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