Aeroacoustic validation of the free wake method first on the basis of a H145 main rotor in descent flight

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dc.contributor.authorKranzinger, P.P.
dc.contributor.authorKessler, M.
dc.contributor.authorKrämer, E.
dc.date.accessioned2018-10-22T08:26:07Z
dc.date.available2018-10-22T08:26:07Z
dc.date.issued2016
dc.identifier.otherERF2016_155_P. KRANZINGER_P
dc.identifier.urihttp://hdl.handle.net/20.500.11881/3757
dc.language.isoen
dc.subject.otherAerodynamics
dc.titleAeroacoustic validation of the free wake method first on the basis of a H145 main rotor in descent flight

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